N412UA

Part: RESERVOIR — LOW (HYD SYSTEM) · airframe 90,286 hrs · 34,670 cycles

ECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - HYD OCCURED IN CRUISE.QUANTITY NORMAL AND BRAKEACCUMULATER LEVEL DID NOT DECREASE. PER POST FLIGHT REPORT AFS1 MESSAGE HYDRAULIC YELLOW 3151 GN - SYSTEM PRESSURE SWITCH FAULT. REMOVED AND REPLACED 3151 PRESSURE SWITCH REF AMM 29-32-12-400-003-A. OPERATED YELLOW SYSTEM NO MESSAGE OPS CHECKS GOOD.

Part: CHANNEL — CRACKED (EMERGENCY EXIT) · airframe 86,723 hrs · 33,045 cycles

EMERGENCY EXIT DOORS, RH FWD DOOR HATCH, CRACK IN FWD AND AFT CHANNELS INNER STRUCTURE. (A3NB-52-4-6031). REMOVED AND REPLACED R/H FWD EMERGENCY EXIT DOOR FWD AND AFT CHANNELS INNER STRUCTURE IAW A320 SRM 51-42-11 PARA2E. WORK PERFORMED BY V063294, INSPECTED BY Q886, ENTERED BY V927860

Part: SEAT TRACK — CORRODED (FRM 20) · airframe 86,723 hrs · 33,045 cycles

A3NB-25-3-6110, R/H FWD OF 1ST ROW FR20 SEAT TRACK AT -Y1292 HAVE SIGN OF CORROSION REQ EVALUATION. REF BY PEMCO NR. 11085.0100. REPAIRED CORRODED SECTION OF -Y1292 SEAT TRACK AT FR20 IAW A320 SRM 53-11-15-300-008.

Part: DOOR — CRACKED (EMERGENCY EXIT) · airframe 86,723 hrs · 33,045 cycles

EMERGENCY EXIT DOORS, LH FWD DOOR HATCH, CRACKS IN AFT CHANNELS INNER STRUCTURE. (A3NB-52-4-6031). REF BY PEMCO NR.11085.0287. REMOVED AND REPLACED AFT SEGMENT L/H FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-42-11 PARA 2E.COMPPLETED BY V063294, INSP BY Q957 ENTERED BY V928371. JOB HAS BEEN ACCOMPLISHED. COMPLETED BY Q957, ENTERED BY V928371 . INSP BY Q957. RE-INSP BY Q966.

Part: CONTROLLER — FAILED (CABIN TEMP) · airframe 86,714 hrs · 33,041 cycles

SD BLEED PAGE SHOWSAMBER XX FOR PACK1 OUTLET TEMP.PACK1 BYPASS V ALVE POS. PACK COMP OUTL LOCKED PER TOMC. H CASTRO ITEM UNLOCKED BY TOMC REPLACED PACK 1 TEMP CONTROLLER 7HH PER AMM 21-61-34. OPS CHECK WAS GOOD AT THIS TIME

Part: SKIN — DENTED (FRAME 15) · airframe 84,634 hrs · 32,143 cycles

UPPER FUSELAGE FWD OF THE L1 DOOR WAS DENTED AT FRAME 15. EVALUATED DENT IAW SRM 53-00-11-283-005. DENT MEASURES 1.1"X1.1" X .020" DEEP. DENT IS IN RIVETED STIFFENED AREA AND IS CATEGORY C. DENT MUST BE REPAIRED WITHIN 200 FLIGHT CYCLES IAW PARAGRAPH 2.A.(1) AND FIGURES 001 AND 002. REPAIRED IAW SRM 53- 11-13-02A PAGE 2 OF 7, INSTALLED DOUBLER IAW SRM 53-00-11-300-043.

Part: RECTIFIER — MALFUNCTIONED (NR 2) · airframe 83,762 hrs · 31,753 cycles

TR UNIT #2 OUTPUT FLUCTUATING CAUSING MULTIPLE OTHER ISSUES WITH FAC2, SEC3, FMGC2, EMER LIGHTING ETC. ETC., SEE LOG 3469940 FOR SIMILAR HISTORY. REPLACED TR2 PER AMM 24-32-51. AFTER 20-30 MIN OBSERVED TR2 VOLT AGE INTERMITTENLY DROPPING TO LOW 20''S VDC AND TRUNING AMBER ON DISPLAY. CABIN LIGHTS BEGAN TO FLICKER AND TURN OFF, ALONE WITH FAC2, FMGC2 AND FCU2. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1222257 SN OFF 4737 RECTIFIER, TRAN OFF 31-2431-9-0002 4737 ON 31-2431-9-0002 0957 OR BASE (PART# 620SE01) REF IPC 24-32-08-02 ITM 80. FOUND "B" PHASE CONNECTION BURNT ON CONTACTOR 14PU. NEED CONTACT RPL CONTACTOR 14PU AND ASSOCIATED BASE.REF MM24-32-55. NO HELP. RESET TR TWICE, TRIPPED BOTH TIMES. REF MM24-32-51. REPLACED CONTACTOR 5PU2 REF MM24-32-55, NO HELP. REPLACED TR2 RECTIFIER, TRAN OFF 31-2431-9-0002 0957 ON 31-2431-9-0002 4959 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1302720 SN OFF 0957 OPERATIONAL TEST OF DC GENERATION SWITCHING OK PER MM 24-32-00-710-001-A.

Part: PRESSURE PANEL — CRACKED (FR36) · airframe 83,026 hrs · 31,434 cycles

EA 5330-05216 OP 001 L/H AIR COND BAY FR36 Y + 1292.0 PRESSURE PANEL CRACKED OUTSIDE THE CUT-OUT AREA. (REF NR 99842273) ACCOMPLISHED CENTER FUSELAGE FR-35 TO FR-36 MILLED PANEL REPAIR IAW AC 4712 EC/RA 5330-06595.

Part: GIRT BAR — OBSTRUCTED (R2 DOOR) · airframe 78,470 hrs · 29,357 cycles

IN FLIGHT 2R SLIDE SHOWED NOT ARMED. F/A PUSHED HANDLE TO REARM. CLEANED AND REMOVED DEBRIS FROM GIRT BAR, CYCLED DOOR MULTIPLE TIMES NOT DEFECTS NOTED. AC OK FOR SERVICE.

Part: FITTING — DEBONDED (RUDDER) · airframe 77,657 hrs · 28,980 cycles

RIGHT LOWER AFT HOIST POINT DISBONDED AND LOOSE. REPAIRED THE RUDDER IAW TD 80340786/005 A AND SRM 51-77-11.

Part: DIAPHRAGM — FAULTY (R1 DOOR BOTTLE) · airframe 77,657 hrs · 28,980 cycles

R1 DOOR DAMPER ASSIST BOTTLE PRESSURE CHECK FOUND TO BE LOW AFTER PREVIOUS SERVICING. REMOVED AND REPLACED R1 DOOR DAMPER PERCUSSION MECHANISM DIAPHRAM AND SEALS IAW AMM 52-10-00-610-001-A. NO LEAKS NOTED.

Part: FITTING — CORRODED (LT MLG) · airframe 77,657 hrs · 28,980 cycles

LEFT MLG ACTUATOR ANCHORAGE FITTING HAS CORROSION ON UPPER SURFACE AT 5:00 POSITION. REPAIRED CORROSION ON LH MLG ACTUATOR ANCHORAGE FITTING UPPER SU RFACE IAW A320 SRM 57-26-13-300-009. FABRICATED 1EA BUSHING IAW A320 SRM 57-26-13-300-009 BUSHING O/D 4.152,ALSO FABRICATED 2 EA WASHERS IAW SRM 57-26-13-300-009, PG 5 STEPS Y AND Z. INSTALLED BUSHING AND WASHERS IAW SRM 57-26-13-300-009, PG 5 STEP AD.

Part: FITTING — CORRODED (FRAME 26) · airframe 77,657 hrs · 28,980 cycles

FWD CARGO BAY, TWO INCHES FWD OF FRAME 26 2IN OTBD OF STRINGER 41R FITTING CORRODED. REPAIRED FWD CARGO FITTING IAW SRM 53-00-11-300-022.

Part: DOOR SILL — CORRODED (FRAMES 24-28) · airframe 77,657 hrs · 28,980 cycles

FWD CARGO INNER DOOR SILL CORRODED AT NUMEROUS LOCATIONS. REMOVED AND REPLACED IAW SRM 51-72-11 P.1-2.

Part: DOOR FRAME — CRACKED (FRM 68) · airframe 77,657 hrs · 28,980 cycles

LEFT AFT PASSENGER DOOR CUTOUT, FRAME 68 DOOR STOP FITTING NR 7 INBOARD LOWER HOLE IS CRACKED AT 12:00 AND 6:00. CRACK AT 6:00 MEASURES APPROX. 14 INCHES FROM FORWARD LOWER EDGE OF HOLE. CRACK AT 12:00 CANNOT BE MEASURED FROM FORWARD SURFACE. LT AFT PAX DOOR CUTOUT FRAME 68 DOOR STOP FITTING NR 1 INBD LOWER HOLE INSTALLED REPAIR FITTING IAW SRM 53-41-12-300-011.

Part: STRINGER — CORRODED (FRAMES 30-31) · airframe 77,657 hrs · 28,980 cycles

FWD CARGO BAY RIGHT AT FRAMES 30 - 31, STRINGER 41R CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-11, P1.

Part: FITTING — CORRODED (R1 DOOR) · airframe 77,657 hrs · 28,980 cycles

R1 DOOR FWD CUTOUT LOWER CORNER FITTING CORRODED. REMOVED & REPLACED FWD LWR CORNER FITTING AT R1 DOOR FRAME 16 IA W A320 SRM 51-42-11

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 77,657 hrs · 28,980 cycles

FWD CARGO UNDER FLOOR AREA AT FRAME 31 BETWEEN STRINGERS 40L-41L SHEAR TIE CORRODED. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-42-11, PG 12.

Part: SHEAR TIE — CORRODED (FRAME 27) · airframe 77,657 hrs · 28,980 cycles

FWD CARGO UNDER FLOOR AREA AT FRAME 27, STRINGERS 43 & 44L, SHEAR TIE HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-42-11 P.12.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 77,657 hrs · 28,980 cycles

FWD CARGO UNDER FLOOR AREA AT FRAME 31, STRINGER 43 - 44L SHEAR TIE CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-42-11, P.1.

Part: STRINGER SPLICE — CORRODED (FRAME 30-31) · airframe 77,657 hrs · 28,980 cycles

FWD CARGO UNDER FLOOR AREA BET. FRAMES 30-31, STRINGER SPLICE 43L HAS CORROSION . REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-72-11. P.2.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 77,657 hrs · 28,980 cycles

FWD CARGO UNDER FLOOR UNDER AREA AT FRAME 31, STRINGERS 40-41RT SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-42-11, P.12.

Part: DOOR SILL — CORRODED (FRAME 68) · airframe 77,657 hrs · 28,980 cycles

AFT CABIN PAX DOOR SILL FRAME 68, STRINGER 23L HAS CORROSION. REMOVED CORROSION AND FOUND TO BE BEYOND LIMITS IAW SRM 53-41-79-283-002. INSTALLED A NEW DOOR SILL IAW SRM 51-72-11-911-001, REV 118.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 77,657 hrs · 28,980 cycles

FWD CARGO UNDER FLOOR AREA AT FRAME 28 BETWEEN STRINGERS 41 AND 42R SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 5742-11 P. 12.

Part: PLATE — CORRODED · airframe 77,657 hrs · 28,980 cycles

LAVATORY EXHAUST VENT REINFORCEMENT PLATE CORRODED. REMOVED AND BLENDED THE CORROSION ON THE LAV EXHAUST VENT REINFORCEMENT PLATE, FOUND TO BE OUT OF LIMITS IAW SRM 51-73-11-001. REMOVED AND REPLACED LAVATORY EXHAUST VENT REINFORCEMENT PLATE IAW SRM 51-7 2-11-911-001.

Part: DOOR SILL — CORRODED (FRAME 68) · airframe 77,657 hrs · 28,980 cycles

L2 DOOR SILL AT FRAME 68 HAS CORROSION UNDER GIRT BAR PLATE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14-283-002, REV 119, INSTALLED A NEW DOOR SILL IAW SRM 51-72-11-911-001 REV. 118, 51- 42-11-001. REV. 118.

Part: FITTING — CORRODED · airframe 77,657 hrs · 28,980 cycles

L1 DOOR CUTOUT FWD LOWER CORNER FITTING HAS CORROSION. REMOVED & REPLACED THE FITTING IAW SRM 51-72-11 -911-001.

Part: STRINGER — CORRODED (FRAMES 29-33) · airframe 77,657 hrs · 28,980 cycles

FWD CARGO BAY, UNDER FLOOR AREA FRAMES 29-33, STRINGER 41R HAS CORROSION. REMOVED AND REPLACED THE STRINGER IAW SRM 51-72-11-911-002.

Part: CLEAT — CORRODED (FRAMES 56-57) · airframe 77,657 hrs · 28,980 cycles

AFT CARGO BAY, FRAMES 56 - 57, STRINGERS 41L-42L CLEAT HAS CORROSION. REMOVED AND REPLACED IAW SRM 51-42-11, PARA F.

Part: THRESHOLD — CORRODED (FRAMES 52-56) · airframe 77,657 hrs · 28,980 cycles

AFT CARGO DOOR THRESHOLD COVER SHEET HAS CORROSION FRAMES 52-56. REMOVED AND REPALCED THE COVER SHEET IAW SRM 51-42-11, PAR E.

Part: DOOR FRAME — CORRODED (R2 DOOR) · airframe 77,657 hrs · 28,980 cycles

R2 DOOR JUST ABOVE AFT GIRT BAR FITTING ATTACH, LOWER DOOR FRAME HAD SURFACE CORROSION. FABRICATED AND INSTALLED A REPAIR FITTING IAW SRM 53-41-12-300-001, FIG 20101.

Part: STRINGER — CORRODED (FRAMES 55-57) · airframe 77,657 hrs · 28,980 cycles

AFT CARGO BAY FRAMES 55-57, STRINGER 42L HAS CORROSION. REMOVED AND REPLACED THE STRINGER IAW SRM 51-72-11, PG 2.

Part: FITTING — CORRODED (NR 2 NACELLE) · airframe 77,657 hrs · 28,980 cycles

NR 2 PYLON SPIGOT BEARING AND BEARING FITTING HAS HEAVY SUFACE CORROSION. REMOVED AND REPLACED THE NR 2 PYLON SPIGOT BEARING FITTINGS IAW SRM 54-51-12-300-001, REV 119. SPIGOT BEARING BALL JOINT INSTALLS ON ROUTINE CARD 18-5451-1-2715

Part: FITTING — CORRODED (L1 DOORWAY) · airframe 77,657 hrs · 28,980 cycles

L1 DOOR CUTOUT AFT LOWER CORNER FITTING HAS CORROSION. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-13, REV 118. REMOVED AND REPLACED THE FITTING IAW SRM 51-72-11-911-001, REV 118.

Part: SUPPORT — CORRODED (FRAMES 69-70) · airframe 77,657 hrs · 28,980 cycles

LEFT FRAME SUPPORT FRAMES 69 - 70 CORRODED. REMOVED CORROSION AND FOUND TO BE BEYOND LIMITS, REMOVED AND REPLACED THE SUPPORT IAW SRM 51-74-11-001, PAR 4, 51-73-11-0, 01, PG 4, AND 51-72-11-911-001, PG 1,2.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 76,175 hrs · 28,311 cycles

EMERGENCY EXIT LTS ALL ON IN ARMED SWITCH POSITION CYCLED EMERG. LIGHT SWITCH EMERG LIGHTS OPS CHECK NORMAL OK TO CONTINUE.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 71,745 hrs · 26,332 cycles

SEATS 29DEF O2 MASKS HANGING DOWN. INSPECTED CONTAINER & DOOR, NO DAMAGE NOTED. REPACKED O2 MASKS AMM TASK 35-23-00-550- 003.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 69,879 hrs · 25,567 cycles

EXTRACT FAULT DISPLAYED ON UPPER ECAM SCREEN. ELEC FUMES FOLLOWED BY VENT EXTRACT FAULT, TURNED OFF BLOWER EXTRACT CABIN FANS NO FUMES. REPLACED EXTRACT FAN 18HQ IAW AMM 21-26-51. COMPLETED OPERATIONAL TEST OF EXTRACT & BLOWER FANS IAW AMM 21-26-51-710-001-A. NO FAILS AT THIS TIME.

Part: DOUBLER — DEBONDED (FUSELAGE) · airframe 68,252 hrs · 24,949 cycles

AFT LT FUSE AFT OF FR 77 STRINGER 29L - 30L PREVIOUS REPAIR DOUBLER DISBONDED. INSTALLED NEW REPAIR DOUBLER IAW SRM 53-51-11 NO SRI IAW 53-51-11 TBL 202.

Part: BATTERY — FAILED (CABIN) · airframe 67,445 hrs · 24,631 cycles

EMERGENCY LIGHT FWD LT BATTERY TESTS BAD DURING 2 SV EMERGENCY LIGHT TEST. REPLACED BATTERY IAW MM 33-51-04 OPERATIONS CHECKED OK.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 67,357 hrs · 24,599 cycles

CABIN FAN FAULT CAME ON COND PANEL.

Part: WIRE HARNESS — FAULTY (NLG) · airframe 67,280 hrs · 24,567 cycles

LGCIU 2 FAULT DISPLAYED ON UPPER ECAM SCREEN LG. R & R THE NLG ELECTRICAL HARNESS 2M IAW AMM, OPERATIONS CHECKED NORMAL.

Part: RELAY — FAILED (LANDING GEAR) · airframe 67,123 hrs · 24,513 cycles

LGCIU 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. RESET IAW PROC, RETURNED AGAIN. ITEM ROLLED FORWARD. REPLACED WHEEL SPEED RELAY 24GG IAW A320 AIRCRAFT SCHEMATIC MANUAL 32-31-04. PERFORMED A TAXI TEST OF THE AIRCRAFT TO CONFIRM FIX. OPERATION CHECKED GOOD. NO LGICU2 FAULT MESSAGE DISPLAYED.

Part: PANEL — UNSECURE (CABIN) · airframe 67,080 hrs · 24,498 cycles

AFT FLIGHT ATTENDANT JUMP SEAT O2 MASK PANEL AJAR AND WILL NOT SECURE SHUT. INOPERATIVE AFT FLIGHT ATTENDANT SEAT & PLACARDED 38C & 38D FOR FLIGHT ATTENDANT USE ONLY. PLACARDED AFT FLIGHT ATTENDANT JUMP SEAT INOPERATIVE.

Part: HYDRAULIC LINE — LEAKING (LT WING) · airframe 66,953 hrs · 24,455 cycles

FOUND HYD LINE LEAKING ON LT WING FWD INBD FLAP OTBD ACTUATOR. REPLACED YELLOW HYD SYS PRESS LINE. NEED TO ACCOMPLISH LEAK CHECK.

Part: FDU — FAULTY (APU) · airframe 66,896 hrs · 24,437 cycles

APU FIRE DET WILL NOT TEST. IAW MEL, REPLACED APU FDU, TESTED OKAY.

Part: GENERATOR — MALFUNCTIONED (NR 2) · airframe 66,886 hrs · 24,432 cycles

NR 2 GENERATOR ELECTRICAL ISSUE, FLT DIVERTED.

Part: LEVER — LACK OF LUBE (NR 2 ENGINE) · airframe 66,570 hrs · 24,319 cycles

ENGINE 2 THRUST LEVER IS DIFFICULT TO GET OUT OF REVERSE, ITS STICKING WHILE MOVING TO IDLE. LUBED THRUST LEVERS, OPERATIONS CHECKED NORMAL.

Part: SHAFT — SHEARED (ENGINE STARTER) · airframe 66,520 hrs · 24,298 cycles

CONT MAX N1 WAS 8 PERCENT BOTH STARTS. REPLACED ENGINE STARTER, FOUND SHAFT SHEARED, REPLACED ENGINE START VALVE. OPERATIONS CHECKED. START 3 TIMES ALL GOOD.

Part: PLATE — DAMAGED (NR 5 SLAT) · airframe 66,370 hrs · 24,240 cycles

NR 5 SLAT CLOSING PLATE DAMAGED. REMOVED DAMAGED SLAT CLOSING PLATE, OPERATED SLATS. ALL OK.

Part: OXYGEN MASK — NO TEST (COCKPIT) · airframe 66,076 hrs · 24,119 cycles

CAPTAIN'S FWD O2 MASK WILL NOT TEST PROPERLY. AIR WILL KEEP FLOWING WHEN MASK SWITCH IS PUT IN EMERGENCY POSITION. REPLACED MASK, OPS CHECKED OK.

Part: O-RING — FAILED (POT WATER LINE) · airframe 66,027 hrs · 24,097 cycles

LARGE AMOUNTS OF WATER LEAKING FROM UNDER THE AIRPLANE. FOUND POTABLE WATER TANK DISTRIBUTION LINE O-RING BLOWN. REPLACED O-RING, OPS AND LEAK CHECKED GOOD.

Part: MICROPHONE — INOPERATIVE (COCKPIT) · airframe 65,990 hrs · 24,086 cycles

CAPT HAND-MIC INOPERATIVE. PLACARDED HAND MICROPHONE INOPERATIVE. BOOM SET OPS CHECKED OK. REPLACED MICROPHONE ASSY WITH SPARE FOUND ON ACFT.

Part: CONTROL BOX — FAILED (NLG STEERING) · airframe 65,957 hrs · 24,069 cycles

STEERING DISCONNECT MESSAGE DISPLAYED AFTER PUSHBACK. R & R NLG LOCKOUT BOX, OPS CHECKED GOOD.

Part: SENSOR — FAULTY (INLET PRESSURE) · airframe 65,507 hrs · 23,895 cycles

LOW APU PRESSURE ON START. 8 PSI. HAD TO BOOST APU TO START. SUP: AFTER DE-BRIEF CREW, THEY HAD GOOD PRESSURE UNTIL THEY ATTEMPTED AN ENGINE START IN AUTO. THE PRESSURE SLOWLY DROPPED TO 8 PSI WHEN THEY INITIATED AN APU BOOST TO RECOVER THE LOW PRESSURE. REPLACED THE INLET PRESSURE TEMP SENSOR APS 3200. APU BLEED PRESSURE NORMAL.

Part: PAINT — CHIPPED (NR 2 COWLING) · airframe 65,463 hrs · 23,874 cycles

CREW REPORT: LARGE CHIPPED PAINT AREA ON FORWARD OUTER COWLING IN THE 9 O'CLOCK POS FACING NR 2 ENGINE REPAIRED PAINT.

Part: SEAT — DEFECTIVE (COCKPIT) · airframe 65,361 hrs · 23,833 cycles

F/O SEAT FWD AFT HAS A GRINDING FEEL ON THE TRACK BOTH WITH MANUAL AND ELECTRONIC FUNCTION. REPLACED FO SEAT ASSY PER MM, OPS CHECK GOOD.

Part: COVER — LOOSE (L2 DOOR SLIDE) · airframe 65,071 hrs · 23,716 cycles

L2 DOOR SLIDE COVER LOOSE. SECURED SLIDE COVER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,047 hrs · 23,706 cycles

AFT LAV EMERGENCY LIGHT INOP. RELAMPED, OPS NORMAL.

Part: GIRT BAR — OBSTRUCTED (L1 DOOR) · airframe 64,898 hrs · 23,641 cycles

L1 DOOR ARMING LEVER SEEM SPONGY. ALL ARMING INDICATIONS APPEAR NORMAL. CLEANED GIRT BAR CATCHES AND GIRT BAR ENDS OF EXCESSIVE DEBRIS. CLOSED AND ARMED ALL ENTRY DOOR AND PRESSURIZED ACFT UP TO 2.1 PSI. NO ECAM MESSAGES NOTED.

Part: PANEL — FAULTY (COCKPIT) · airframe 64,783 hrs · 23,598 cycles

NR 2 ENGINE NR 2 BOTTLE DISCHARGE LIGHT ILLUMINATED. IF RESET PANEL LIGHT GOES OUT BUT COMES BACK WITH FIRE TEST. VERIFIED INTEGRITY OF FIRE BOTTLE 8WE2 FROM 1WDC TO 8WE2A FROM FIRE PANEL BOTTLE WIRING CHECKS OK. REF ASM 26-21-01. PANEL 330TS08Y 565-9002 REF IPC26-12-08-01 ON ORDER. REPLACED AND TESTED ENGINE -APU FIRE PANEL.

Part: SCREW — WRONG PART (DOOR FRAME) · airframe 64,716 hrs · 23,575 cycles

TWO SCREWS ARE LOOSE ON UPPER PART OF COCKPIT DOOR FRAME ON COCKPIT SIDE OF FRAME. SCREWS SHANKED OUT. REPLACED SCREWS COCKPIT DOOR, OPS NORMAL

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 22 DEF) · airframe 63,906 hrs · 23,254 cycles

O2 MASK DEPLOYED AT SEATS 22DEF. RESTOWED MASK AT ROW 22DEF. NO FURTHER DEFECT NOTED. PER MT35-003.

Part: COVER — UNSECURE (R2 DOOR) · airframe 63,880 hrs · 23,246 cycles

SLIDE COVER DOOR 2R IS AJAR. SECURED SLIDE COVER.

Part: WINDOW — STUCK (COCKPIT) · airframe 63,603 hrs · 23,142 cycles

CREW REPORT: CAN'T CLOSE CAPT WINDOW. FREED STUCK WINDOW ASSY, INSPECTED WINDOW MECHANISM; NO DAMAGE NOTED.

Part: CONTROL CABLE — FAILED (RUDDER PEDAL) · airframe 63,504 hrs · 23,112 cycles

FIRST OFFICER'S RUDDER PEDAL ADJUSTMENT KNOB INOPERATIVE. -CABLE BROKE FROM THE LEVER, UNABLE TO ADJUST THE RUDDER PEDALS AT ALL. REPLACED CABLE PER MM.

Part: BATTERY — FAULTY (MAIN) · airframe 63,486 hrs · 23,104 cycles

CREW REPORTS NR 1 BATTERY SHOWS 24 VOLTS. REPLACED NR 1 SHIPS BATTERY.

Part: TIRE — DEFECTIVE (NLG) · airframe 63,177 hrs · 22,971 cycles

NOSE LANDING GEAR VIBRATION DURING TAKEOFF. MODERATE NOSE WHEEL VIBRATION AFTER LIFTOFF. REPLACED NOSE GEAR TIRES DUE TO VIBRATION.

Part: SKIN — DENTED (FUSELAGE) · airframe 63,142 hrs · 22,956 cycles

SKIN DENTED BETWEEN FRAMES 22-23 AND S22-23L REPAIR ACCOMPLISHED IAW SRM 53-11-11 FIG 212.

Part: VALVE — FAULTED (RT A/C PACK) · airframe 62,902 hrs · 22,871 cycles

PACK 2 FAULT, RTFL. PERFORM OPS CHK OF PACK 2 TEMP SYS REF AMM 21-61-00-710-001-A. OPS CHK SYS NORMAL NO FAULTS NOTED. FAULT REOCCURED BEFORE SUCC FLT. FOUND PACK VALVE WOULD OPEN , BUT NO INDICATION ON ECAM, REPLACED RT PACK VALVE PER MM. NO FAUILTS. OPS CHECKED OKAY.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 62,775 hrs · 22,827 cycles

FLAPS LOCKED, ALIGNMENT FAULT DISPLAYED ON UPPER ECAM SCREEN F-CTL. TROUBLESHOT REF MT AND TSM TASK. RT APPU WAS OUT OF TOLERANCE. REPLACED RT APPU PER MM. RAN FLAPS WITH NO FAULTS.

Part: COMPUTER — FAULTY (NR 2 ELAC) · airframe 61,992 hrs · 22,543 cycles

CREW REPORTS ELAC 2 FAULT ON CLIMB OUT OF DEN. 2ND REPEAT FAULT. REPLACED NR 2 ELAC. ALL TESTED OK INCLUDING SIDE STICK OPS, REF AMM 27-93-00. ALSO, PERFORMED AFS LAND TEST, 22-97-00.

Part: O-RING — DAMAGED (UPPER BEACON) · airframe 61,641 hrs · 22,415 cycles

HIGH PITCH SOUND IN CEILING AT ROW 20. REMOVED UPPER BEACON ASSY 7LY. FOUND O-RING DAMAGED. REPLACED PACKING ITEM 90 ON IPC PER MM33-48-11. PRESSURIZED A-C NO LEAK AND HIGH PITCH SOUND NOTED.

Part: CAP — DAMAGED (FUEL SYSTEM) · airframe 61,556 hrs · 22,386 cycles

REFUEL COUPLING CAP DAMAGED. REMOVED DAMAGED CAP. COMPLIED WITH CDL. REPLACED CAP.

Part: PIN — MISSING (ESCAPE PANEL) · airframe 61,301 hrs · 22,300 cycles

D' RING MISSING ON COCKPIT DOOR FOR PIN IN ESCAPE PANEL. REMOVED AND REPLACED OUTBOARD PIN, OPS GOOD.

Part: TRANSMITTER — FAULTY (BRAKE SYSTEM) · airframe 61,060 hrs · 22,204 cycles

CREW COMMENTS: GOT BRAKES AUTO BREAK FAULT ECAM AFTER TAKEOFF. AUTO BRAKE FUNCTION INOP - BRAKES. EXTENSIVE HISTORY OF BRAKE SYSTEM 1 FAULTS. COMPLIED WITH MEL AFTER ACCOMP PFR. SUSPECT BRAKE PETAL XMITR 565-9200 NIL DEN. TROUBLESHOT PER TSM. AC TROUBLESHOOTING DATA FAULTS STEP 4.A.3 SEVERAL TIMES. REF HISTORY BSCU & XMITTER (9GG) HAVE BEEN CHG'D. ORIGINALLY HITTING SYS 2 UNTIL XMTR (9GG) RPLD 10JAN, NOW HITTING SYS 1. AFTER ACP WIRING CKS & EVALUATING TSD AS NOTED, RPL XMTR (9GG) PRECAUTIONARY.

Part: OXYGEN SYSTEM — LEAKING (COCKPIT) · airframe 60,678 hrs · 22,061 cycles

CREW OXYGEN SYSTEM LOW 1120 PSI. FOUND SLIGHT LEAK AT F/O O2 MASK BOX AND BOX WOULD TEST INTERMITTENTLY. REPLACED BOX AND MASK ASSY.

Part: LIGHT — FAULTY (EXTERIOR) · airframe 60,542 hrs · 22,009 cycles

EMERGENCY LIGHT TEST SHOWS EXT LOADS EMERGENCY RT FAULT. RELAMPED RT AFT EXT OVERWING EMERGENCY EXIT LIGHT, CHECKED OK.

Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 60,487 hrs · 21,990 cycles

WX RADAR FAILURE, RTFL WX RADAR INOP: CAPTS SCREEN PAINTS RED AND F-O SCREEN PAINTS PURPLE. ATTEMPTED RESET IN FLIGHT AND NO HELP. DEBRIEFED CREW. PWR SYSTEM UP GOT RT FAIL MESSAGE ON BOTH SCREENS. REPLACE WX TRANSCEIVER IAW AMM. OPS CHECK'D NORMAL. BITE CHECKED GPWS SYSTEM, ALSO NO FAULTS.

Part: SENSOR — FAULTY (BRAKE SYSTEM) · airframe 60,407 hrs · 21,961 cycles

NR 3 BRAKE HIGH TEMP IND, RTFL. AFTER PLR REVIEW FOUND SEVERAL HITS ON BSCU2 (NO BSUU2 DATA (INTM) 32-42-34 OUT OF STOCK ON BSCU. CALLED SAMC C FOR VERIFICATION OF MISMATCH OF MR NUMBERS BUT THE BENCH PLUGS DO NOT MATCH. REINSTALLED OLD UNIT MR62924 NEW UNIT MR62964 DOES NOT FIT (PARTS: 565-9020 MR62964 UNIT LOB: N. -INF- :IAD BSCU MR62964 NOTED ABOVE TAGGED W-RFU AND RETURNED TO JL AS POSSIBLY MIS-KEYED. REPLACED NR 3 BRAKE TEMP SENSOR AND RT GEAR BRAKE TEMP MONITORING UNIT, TESTED OK. BSCU MR62924 (P/N C202163392E35) INSTALLED.

Part: LATCH — BROKEN (O2 MASK DOOR) · airframe 59,415 hrs · 21,547 cycles

SEAT ROW 20-D, E, F OXYGEN MASKS DOOR LATCH BROKEN. DF PER MEL REF: 3521A,SEAT ROW 20 D, E, F NOT TO BE OCCUPIED. -CQT- :PART NUMBER FOR NEW MODULE IS AJ5R34-25. NEXT STATION, CONFIRM PARTS NEEDED AND IPC REFERENCE. SUSPECT IPC 35-21 (PCN 649-2749). NEXT STATION UPDATE. :REFERENCE VERIFIED CORRECT. PARTS: 649-2749 2M1133-25 (CONTAINER ASSY). REBONDED LATCH RELEASE PIN TO DOOR. DOOR IS SECURE,ACP O2 MASK DROP CHK. TESTS OKAY. SEAT ROW RETURNED TO NORMAL USE.

Part: RECEPTACLE — OUT OF TOLERANCE (LT OVRWING SLIDE) · airframe 59,103 hrs · 21,433 cycles

LEFT OVERWING SLIDE HAS TWO UPPER MIDDLE SCREWS PROTRUDING OUT. WILL NOT TIGHTEN IN RECEPTACLE. REPLACED AFFECTED LT OVERWING SLIDE PANEL SCREW MOUNTING RECEPTACLES.

Part: FILTER — DIRTY (CABIN) · airframe 58,673 hrs · 21,246 cycles

MUSTY SMELL IN CABIN. DUE TO CABIN HAVING STRONG ODOR FROM APU RUNNING THE A-C PACKS, AS PER OPB, PAX FILTER FOR RECIRCULATION TO BE REPLACED ON BOTH SIDES (FIN#4012HM & 4013HM). REMOVED & REPLACED THE CARTRIDGE FILTER POSITION 4012HM AND 4013HM. OK FOR SERVICE.

Part: HOOK AND LOOP — UNSECURE (EVAC SLIDE) · airframe 58,477 hrs · 21,173 cycles

CREW REPORT: SLIDE PACK COVER AT 2L HAS FALLEN OFF. RE-SECURED BUZZLE, FOUND VELCRO ON TOP UNGLUED. RESECURED WITH DOUBLESIDED TAPE AS INTERIM.

Part: CONTROL UNIT — FAULTY (SMOKE DETECTOR) · airframe 58,034 hrs · 20,998 cycles

SDCU MAINTENANCE STATUS CLASS II MESSAGE DISPLAYED ON LOWER ECAM. DEFERRED PER PDL. INSTALLED NEW SDCU PER MM, OPS CHECKED GOOD.

Part: ATTACH ANGLE — CRACKED (A/C BAY) · airframe 57,332 hrs · 20,702 cycles

LT AC BAY INBD MOST VAPOR BARRIER ATTACH ANGLES HAVE CRACKS. (BARRIER CONTACTS SLAT DRIVE TUBE WHEN INFLATED). FAB NEW FWD BRKT REF DWG D57910289 AND AFT BRKT REF DWG D57910149 AND INSTALLED BOTH.

Part: SUPPORT BRACKET — CRACKED (A/C BAY) · airframe 57,332 hrs · 20,702 cycles

RT AC BAY INBD MOST VAPOR BARRIER SUPPORT ANGLE HAS CRACKS, RBL10. (VAPOR BARRIER CONTACTS SLAT DRIVE ROD WHEN BARRIER INFLATED). FAB NEW BRACKET AND INSTALLED. FABRICATED NEW AFT BRACKET D57910149 AND INSTALLED.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,332 hrs · 20,702 cycles

FUSELAGE DENT AT FR10 JUST BELOW CAPT'S NR3 WINDOW. MAJOR REPAIR ACCOMPLISHED: FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR WITH BLIND FASTENERS IAW SRM. INSTALL PERMANENT REPAIR WITHIN 3000C OR AT HMV3 VISIT DUE 12DEC10. NR P6585V BY NR308152 AND INSPECTED BY LC81. INSTALLED PERMANENT REPAIR PER SRM. REPAIR ACP ON WU L5483H BY MAE MECH NR02969 AND INSP NR 19.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 57,132 hrs · 20,608 cycles

FLOOR PROXIMITY EMERGENCY ESCAPE PATH SEAT MOUNTED LIGHTS CABLE HAS A WIRE BROKEN. CABLE THATS FROM THE FLOOR TO THE SEATS. (SEATS 16ABC). REPLACED SEAT WIRE HARNESS, OPS CHECK GOOD.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,132 hrs · 20,608 cycles

SEAT MOUNTED FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING LIGHTS ARE INOP SEATS 12ABC. REPLACED SEAT WIRE HARNESS AND LIGHT ASSY. OPS CK GOOD.

Part: COVER — DAMAGED (EMERGENCY LIGHTS) · airframe 57,032 hrs · 20,556 cycles

AFT F/A STATION EMERGENCY LIGHT SWITCH COVER DAMAGED. APPLIED INTERIM REPAIR TO LIGHT SWITCH COVER. SWITCH AND COVER STILL USEABLE.

Part: SLIDE — UNSERVICEABLE (L2 DOOR) · airframe 56,201 hrs · 20,182 cycles

DOOR 2L STRAP HANGING FROM SLIDE PACK. WHITE STRAP THAT GOES TO FRONT OF GRIT BAR HAS WORN HOOK AND LOOP. UNABLE TO ATTACH STRAP TO GRIT BAR. DOOR 2 LT MED SLIDE WAS REMOVED FOR SLIDE CHANGE, BUT WAS PUT BACK ON DUE TO NEW SLIDE WAS BAD FROM STOCK. REINSTALLED ORIGINAL SLIDE BACK ON MED 2 LT IAW MM.

Part: BRACKET — OUT OF ADJUST (EMERGENCY EXIT) · airframe 55,760 hrs · 20,006 cycles

R FWD EMERGENCY EXIT DISPLAYED ON UPPER ECAM SCREEN - DOOR. CREW COMMENTS: FWD RT OVERWING EMERG EXIT DOOR OPEN ECAM DURING EARLY TAKEOFF ROLL. ABORTED. REPEAT GRIPE. ADJUSTED BRACKET PANEL ATTACHES TOO, FOR A SECURE FIT. TAKEOFF ROLL AT 20 KNOTS, BRAKE TEMP NORMAL, OK PER REF MM.

Part: BOLT — BROKEN (DOOR 1L SLIDE) · airframe 54,642 hrs · 19,534 cycles

FOUND ON ARRIVAL, DR 1L SLIDE UPPER AFT RETAINING BOLT BROKEN. RPLACED BROKEN RETAINING BOLT. ACCOMPLISHED RII INSPECTION OF THE DOOR 1 LT SLIDE UPPER AFT RETAINING BOLT.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,117 hrs · 19,315 cycles

SKIN HAS HOLE 1" BY 2" LT SIDE JUST FWD OF APU DOOR. MAJOR REPAIR ACCOMPLISHED: ACCESS DOOR PANEL 314AR HAS A CREASE IN IT. PANEL IS LOCATED RT SIDE JUST FWD OF APU DOOR. CUT OUT DAMAGE ON BOTH EXTERNAL & INTERNAL SKIN SECTIONS. RECEIVED EVA FOR THE INTERNAL PILLOW DOUBLER REPAIR. FABRICATED AND DRILLED REPAIR DOUBLER, NEEDS PRIMED AND INSTALLED. PRIMED AND INSTALLED DOUBLER. INSTALLED ACCESS DOOR ASSY.

Part: SEAL — UNSECURE (THRUST REVERSER) · airframe 53,221 hrs · 18,894 cycles

FAIRING UNSECURE, RTFL. REPLACED NR 2 ENG BULL NOSE BULB SEAL. REACTIVATED THRUST REVERSER.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 52,064 hrs · 18,442 cycles

FOUND AIRCRAFT EMERGENCY LIGHTS SW IN ARMED POSITION AND NO POWER ON AIRCRAFT. EMERGENCY LIGHTS BATTERIES ARE DEPLETED. FOUND POWER ON AIRCRAFT AND BATTERIES CHARGED, EMERGENCY LIGHT OP CK'D OKAY.

Part: FITTING — CORRODED (R2 DOOR) · airframe 52,064 hrs · 18,442 cycles

R AFT EMER EXIT DISPLAYED ON UPPER ECAM SCREEN. SLIDE RELEASE MECHANISM IS OUT OF RIG. TRIED ADJUSTMENT. AFT FLOOR FITTING FOUND AT LIMIT OF INBD ADJUSTMENT. CK'D GIRT BAR ADJ ON DOOR. FOUND NO CLEARANCE AT J3 (SHOULD BE .031-.047). REMOVED ROD END FROM TELEFORCE CABLE TO ADJ. FOUND CORROSION ON INTERNAL THREADS, REPLACEMENT ON AOG. HANDLE POPS UP A LITTLE BY ITSELF. REARMS OK. ADJUSTED AFT RT DOOR GIRT BAR FITTINGS & APPLIED SEALANT AS NEEDED.

Part: SENSOR — OUT OF ADJUST (R2 DOOR) · airframe 51,945 hrs · 18,401 cycles

RT AFT SLIDE INDICATION INOP ON DOOR-OXY SYS ECAM PAGE DOOR-OXY. DOOR 2R SLIDE INDICATION WORKS ON THE GROUND BUT NOT AIRBORNE. ADJUSTED SENSOR 7WN2. DOOR INDICATION CHECKS GOOD.

Part: SLIDE — FAULTY (R2 DOOR) · airframe 51,742 hrs · 18,328 cycles

DOOR 2R SLIDE ARMED INDICATION INOP IN FLT. PERFORMED TSM TASK 52-13-0 0-810-809. REPLACED IND LT-SLIDE ARMED ASSEMBLY, AFT R DOOR (3WN 2), AND REPLACED 7WN2 PROX SW HANDLE, R AFT ESC SLIDE. PERFORMED OP-TEST OF EMERGENCY ESCAPE SLIDE RELEASE SYSTEM OF PASSENGER-CREW. TESTED NORMAL.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,511 hrs · 17,121 cycles

SEAT 20 ABC FLOOR PROXIMITY ESCAPE PATH LIGHT IS INOP. FOUND DAMAGED HARNESS. REPLACED HARNESS, OPS CHECKED OK.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 47,863 hrs · 16,903 cycles

EMERGENCY EXIT LIGHTS FLICKERING DURING TAXI IN. UNKNOWN ELECTRICAL (BATTERY) FAULT. REPLACED RT MID CABIN POWER SUPPLY, OPS CHECKED GOOD.

Part: LIGHT — DAMAGED (SEAT 21) · airframe 47,629 hrs · 16,817 cycles

FOUND SEAT 21 EEL DAMAGED. REPLACED DAMAGED SECTION OF EEL SYSTEM. OPS CHECKS ARE NORMAL.

Part: OXYGEN MASK — DAMAGED (COCKPIT) · airframe 46,950 hrs · 16,604 cycles

CAPTAIN'S OXYGEN FACE SHIELD IS DAMAGED. REPLACED DAMAGED O2 FACE SHIELD.

Part: OXYGEN BOTTLE — LOW PRESSURE (27L) · airframe 46,950 hrs · 16,604 cycles

OXYGEN BOTTLE LOW AT 27L. REPLACED O2 BOTTLE AT LOCATION 27L.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 46,394 hrs · 16,391 cycles

FOUND EMERGENCY LIGHTING FAILS 3CK TESTS. 10-19-07 RESET EPSU AND SYSTEM CHECKED GOOD.

Part: ACTUATOR — FAULTED (TRANFER SYS) · airframe 46,373 hrs · 16,384 cycles

FLIGHT DIVERTED DUE TO A FUEL TRANSFER PROBLEM. 10-19-07 FOUND FAULTY NR 2 RIGHT WING TRANSFER VALVE ACTUATOR. REPLACED NR 2 RIGHT WING TRANSFER VALVE ACTUATOR.

Part: COVER — OUT OF POSITION (R2 DOOR) · airframe 45,762 hrs · 16,155 cycles

SLIDE RAFT COVER FELL OFF AT 2R. 09-07-07 SECURED SLIDE COVER.

Part: SOLENOID — MALFUNCTIONED (BLEED AIR SYS) · airframe 45,721 hrs · 16,138 cycles

RTFL DUE TO RIGHT PACK OVERHEAT INDICATION. REPLACED STAT 10HA2, BPRV SOLENOID 10HA2

Part: COVER — OUT OF POSITION (CABIN) · airframe 45,464 hrs · 16,044 cycles

DOOR 2R SLIDE COVER OFF.

Part: PANEL — MALFUNCTIONED (EVACUATION ALARM) · airframe 45,392 hrs · 16,021 cycles

EVAC ALARM SOUNDS INTERMITTENTLY. EVAC PANEL AT 2L,CHECKS NORMAL. AFTER CHECKING THIS PANEL, NO REPEAT INSTANCES HAVE BEEN RECORDED. (SINCE JUNE, 07)

Part: TAB — BROKEN (RH ELEVATOR) · airframe 45,014 hrs · 15,880 cycles

RIGHT ELEVATOR HINGE FITTING NR 1 LWR ANTI-ROTATION TAB IS BROKEN OFF. MAJOR REPAIR ACCOMPLISHED: INSTALLED T-ANGLE REPAIR TO REPLACE ANTI-ROTATION TAB.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 45,014 hrs · 15,880 cycles

LEFT WHEEL WELL LOWER FUSELAGE BELLY FAIRING SUPPORT ANGLE 5 IN LBL IS CRACKED AT FRAME 46. MAJOR REPAIR ACCOMPLISHED: REPLACED KEEL BEAM ANGLE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 45,014 hrs · 15,880 cycles

RIGHT WHEEL WELL LOWER FUSELAGE BELLY FAIRING SUPPORT ANGLE 5 IN RBL IS CRACKED AT FRAME 40. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE.

Part: DOOR — MISINSTALLED (SEAT ROW 23RH O2) · airframe 44,724 hrs · 15,776 cycles

SEAT ROW 23 RT EMERGENCY O2 COMPT DOOR OPENS IN WRONG DIRECTION, HINGE ON INBOARD SIDE. OPEN DOOR CAN IMPEDE EXITING OF PASSENGER IN OUTBOARD SEATS. [SUP 5-1-07] REMOVED AND REINSTALLED DOOR.

Part: HYDRAULIC SYSTEM — READS LOW (GREEN SYSTEM) · airframe 44,523 hrs · 15,701 cycles

GREEN HYDRAULIC LOW LEVEL QTY ECAM ON FINAL. PRESSURE STILL GOOD ON GREEN SYSTEM. EMERGENCY DECLARED. AMBER ALERT. [SUP 06-01-07] PERFORMED A LEAK CHECK WITH ELECTRIC AND ENGINE DRIVEN PUMPS OPERATING AND DID NOT FIND ANY LEAKS. 2 DAYS PRIOR, NR 2 ENGINE DRIVEN PUMP WAS REPLACED. IT WAS ALSO NOTED AS PART OF THE SAME MAINTENANCE ACTIVITY THAT THE YELLOW AND GREEN SYSTEMS WERE OVER SERVICED AND WERE SLIGHTLY DRAINED TO BRING LEVELS WITHIN NORMAL SPECS. SUSPECT THAT TOO MUCH FLUID WAS DRAINED AND/OR DID NOT ACCOUNT FOR NEW EDP NOT BEING FULL OF FLUID YET.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 42,471 hrs · 14,987 cycles

SMOKE/ODOR IN CABIN, LANDED UNDER AMBER, MASKS & ALL SLIDES DEPLOYED. REPLACED NUMBER 1 ENGINE DUE TO OIL WETTING, BURNING AND DEBRIS FOUND AT STAGES 3 & 4 OF HPC.

Part: BULB — MISSING (EMERGENCY LIGHT) · airframe 40,403 hrs · 14,240 cycles

EMERGENCY FLOOD LIGHT ABOVE DOOR 2L HAS ONE BULB MISSING.

Part: ACTUATOR — CORRODED (RT MLG) · airframe 34,032 hrs · 12,073 cycles

RIGHT MAIN LANDING GEAR LOCK STAY ACTUATOR CYLINDER FOUND WITH CORROSION ON THE PORT STATIC SEAL SURFACE. MAJOR REPAIR ACCOMPLISHED. CORROSION REMOVED BY MACHINING AREA AROUND PORT. FOUR LAYERS OF INTERFILL APPLIED TO REWORKED AREA.

Part: LEVER — MALFUNCTIONED (MLG) · airframe 33,596 hrs · 11,930 cycles

WHILE TRYING TO DROP GEAR ON APPROACH, ECAM MSG SHOWED LGCIU 1 AND 2 FAILURE. THIS WAS A POSITIONING FLIGHT. REPLACED LANDING GEAR LEVER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,481 hrs · 10,790 cycles

FUSELAGE SKIN DAMAGED AT FRAME 61 AT STRINGER 40L & STRINGER 41L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FILLERS AND DOUBLER.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 30,481 hrs · 10,790 cycles

DAMAGED FRAME SECTIONS AT FRAME 60 ON STRINGER 40 LT & STRINGER 41 LT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR ON FRAME.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 27,584 hrs · 9,647 cycles

LOWER ECAM MESSAGE HAD AMBER EXIT DOOR WARNING ON DOOR PAGE FOR RIGHT AFT OVERWING DOOR. PROBLEM WAS CAUSED BY MOVEMENT OF THE OVERWING EXIT HANDLE COVER FLAP. REMOVED OVERWING HATCH AND INSPECTED WITH NO FINDINGS. REINSTALLED DOOR AND SECURED DOOR HANDLE COVER FLAP.

Part: THERMOSTAT · airframe 26,126 hrs · 9,094 cycles

#1 ENGINE BLEED FAULT LIGHT ILLUMINATED, HAD BLEED 1OVERHEAT. UNABLE TO RESET SYSTEM. SUPPLEMENTAL DATA UPDATE REPLACED FAN AIR THERMOSTAT, RAN ENGINES, BLEED PARAMETERS NORMAL.

Part: LIGHT — INOPERATIVE (SEAT 9) · airframe 23,904 hrs · 8,324 cycles

EMERGENCY ESCAPE PATH LIGHT AT SEAT 9C IS INOPERABLE. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK OK.

Part: SWITCH — LEAKING (HYDRAULIC SYSTEM) · airframe 20,878 hrs

GREEN HYD RES LO LVL ECAM-GRAVITY GEAR EXTENSION. *S/D* FOUND RESERVOIR TANK FULL. REPLACED GREEN HYD RESERVOIR QUANTITY INDICATOR AND GREEN HYD RESERVOIR LOW LEVEL SWITCH. ALL INDICATIONS NORMAL, NO MSGS.

Part: LINE — LEAKING (RT MLG DOOR)

FLIGHT CREW ACCOMPLISHED MANUAL GEAR EXTENSION DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. AMBER ALERT, NORMAL LANDING. *S/D* FOUND HYDRAULIC LINE AT RIGHT MLG DOOR BYPASS VALVE LEAKING. REPLACED LINE, LEAK CHECK OK.

Part: EEL POWER SUPPLY — INOPERATIVE (CABIN)

AFT EMERGENCY LIGHTS OVER AFT DOORS ARE INOPERATIVE. REPLACED POWER SUPPLY AND OPERATIONALLY CHECKED NORMAL.

Part: SERVO CONTROL — LEAKING (RT AILERON)

HYDRAULIC MOTOR GENERATOR FAILS TEST. TRIES TO COME UP TO SPEED AND THEN SHUTS OFF. REPLACED RIGHT HAND OUTBOARD AILERON SERVO CONTROL DUE TO HIGH INTERNAL LEAKAGE.

Part: DC ELECTRICAL — MALFUNCTIONED (NR 2)

WHEN ACCOMPLISHING THE DC EMERGENCY GENERATION CHECK, TEST FAILS NO ELECTRICAL PARAMETERS. NR 2 ENGINE PARAMETERS APPEAR AND UPPER ECAM SCREEN BLANKS AND SWITCHES TO LOWER SCREEN.

Part: EEL BATTERY — DISCHARGED (CABIN)

LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY.