N402UA

Part: ENGINE — STALLED (NR2) · airframe 86,397 hrs · 33,783 cycles

LEFT ENG COMP STALLSEVERAL JOLTS CLBINGTHRU 13000 FT.. ENG1 SN. V10291 (TSI= 12833) CFDS SHOW ENG1 COMP STALL IN CRZ. WITH VSV MECH/BLD VLV/LPC1. RE. TSM 71-00-00-810-808-A FOR T/SHOOTING AND DISPOSITION. WHQLM-EMC ARSHAD. 08JAN2022. ACCOMPLISHED FUNCTIONAL CHECKS OF #1 ENGINE HPC STAGE 7 SOLENOID ACCOMPLISHED FUNCTIONAL CHECKS OF #1 ENGINE HPC STAGE 7 BLEED ACP ENGINE 1 FADEC SYSTEM TESTS 1A & 1B IAW AMM TASK VALVES 7A,7B AND 7C I/A/W AMM 75-32-51-700-010-A, ALL THREE OPS VALVES I/A/W AMM 75-32-52-700-011-A, VALVES 7A AND 7B PAASSED, 73-22-00-710-040-A, BOTH SYSTEMS PASSED. CHECKS GOOD. VALVE 7C FAILED. REMOVED AND REPLACED #1 ENGINE HPC STAGE 10 SOLENOID VALVE, #1 ENG HPC STAGE 7C VALVE,10HA1 PRV SOLENOID,#1 ENGINE HPC STAGE SOLENOID VALVE 7A,#1 ENGINE HPC STAGE 7 SOLENOID VALVE 7C,STAGE 7 BLEED VALVE. PRESSURE TESTED BURNER SENSE LINE AND PURGE THE BURNER PRESSURE SENSOR LINE. NO LEAKS NO DAMAGE LINE

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,761 hrs · 32,618 cycles

EMERGENCY LIGHTS BATTERY PACK (11WL) FAILS TO ILLUMINATE WITH THE SWITCH IN THE ARM POSITION AND THE C/B'S PULLED, PER HAECO LCQ NON ROUTINE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK, IAW A319/320 MM 38-51-38-000-002A 33-51-38-400-002A OPERATIONS TEST OF THE EMERGENCY POWER SUPPLY UNITS CHECKS GOOD, IAW A319/320 MM 33-51-00-710-001 A AND 33-51-00-710-083A.

Part: INTERCOSTAL — CRACKED (EMERGENCY EXIT) · airframe 83,761 hrs · 32,618 cycles

RT FWD EMERGENCY EXIT DOOR INTERNAL STRUCTURE FWD VERTICAL INTERCOSTAL CRACKED AT FASTENER HOLES. REMOVED AND REPLACED RT FWD EMERGENCY EXIT DOOR INTERNAL STRUCTURE FWD VERTICAL INTERCOSTAL SEGMENT, IAW A320 SRM 51-72-11-911-0 01.

Part: INTERCOSTAL — CRACKED (EMERGENCY EXIT) · airframe 83,761 hrs · 32,618 cycles

RT AFT EMERGENCY EXIT DOOR INTERNAL STRUCTURE FWD VERTICAL INTERCOSTAL CRACKED AT FASTENER HOLES GEN BY V061623 NR9296332 (44332 ) A3NB-52-4-6031 AT HAEC LCQ. REMOVED AND REPLACED RT AFT EMERGENCY EXIT DOOR INTERNAL STRUCTURE FWD VERTICAL INTERCOSTAL SEGMENT, IAW SRM 51-72-11-911-001 BY MECH V929087 INSP BY V061623 PER NR 9296332.

Part: INTERCOSTAL — CRACKED (EMERGENCY EXIT) · airframe 83,761 hrs · 32,618 cycles

LT AFT EMERGENCY EXIT DOOR INTERNAL STRUCTURE FWD VERTICAL INTERCOSTAL CRACKED AT FASTENER HOLES (A3NB-52-4-6031), PER HAECO LCQ NON ROUTINE 9296331 GENERATED BY V061623.

Part: INTERCOSTAL — CRACKED (EMERGENCY EXIT) · airframe 83,761 hrs · 32,618 cycles

RIGHT AFT EMERGENCY EXIT DOOR INTERNAL STRUCTURE AFT VERTICAL INTERCOSTAL CRACKED AT FASTENER HOLE, PER NR9296358 GEN BY V052030. REMOVED AND REPLACED RT AFT EMERGENCY EXIT DOOR INTERNAL STRUCTURE AFT VERTICAL INTERCOSTAL SEGMENT, IAW SRM 51-72-11-911-001 BY MECH V929087 INSP BY N078592 PER NR9296358.

Part: INTERCOSTAL — CRACKED (EMERGENCY EXIT) · airframe 83,761 hrs · 32,618 cycles

LT AFT EMERGENCY EXIT DOOR INTERNAL STRUCTURE AFT VERTICAL INTERCOSTAL CRACKED AT FASTENER HOLES (A3NB-52-4-6031), PER HAECO LCQ NON ROUTINE 9296330 GENERATED BY V061623.

Part: INTERCOSTAL — CRACKED (EMERGENCY DOOR) · airframe 83,761 hrs · 32,618 cycles

LT FWD EMERGENCY INTERNAL STRUCTURE FWD VERTICAL INTERCOSTAL CRACKED AT FASTENER HOLES (A3NB-52-4-6031), PER HAECO LCQ NON ROUTINE 9296328 GENERATED BY V061623.

Part: INTERCOSTAL — CRACKED (EMERGENCY EXIT) · airframe 83,761 hrs · 32,618 cycles

LT FWD EMERGENCY EXIT INTERAL STRUCTURE AFT VERTICAL INTERCOSTAL CRACKED AT FASTENER HOLES (A3NB-52-4-6031), PER HAECO LCQ NON ROUTINE 9296329 GENERATED BY V061623.

Part: SKIN — DAMAGED (FWD CARGO DOOR) · airframe 83,759 hrs · 32,617 cycles

FWD CARGO DOOR DAMAGED BY LADDER. EVALUATED DAMAGE TO FWD CARGO DOOR, IAW SRM52-30-00-283-005 FIG 001. DEPTH .050 LENGTH 1.0 MATERIAL THICKNESS .063. FOUND TO BE OUT OF LIMITS. REPAIRED DAMAGE, IAW SRM 52-31-00-300-010 FIG 001 SHEET 1. THIS IS A CATAGORY A, PERMANENT REPAIR WITH NO RE-INSPECTION REQUIREMENT.

Part: SKIN — CORRODED (RT WING) · airframe 78,748 hrs · 30,399 cycles

RIGHT WING UPPER SURFACE, FROM RIBS 7 - 8, AND 4 INCHES FWD OF WING T /E WAS CORRODED. REPAIRED THE RT WING SKIN IAW ECRA 5725-01012, & REO L21513 REV IR.

Part: DOOR FRAME — CORRODED (FRM 16) · airframe 78,748 hrs · 30,399 cycles

CORROSION WAS FOUND ON THE FWD CABIN R1 DOOR LWR FWD CORNER, FRAME 16 JUST ABOVE THE DOOR SILL. REPAIRED IAW REO-L20420, REV IR, AND ECRA 5310-06995.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 77,113 hrs · 29,695 cycles

R1 DOOR WILL NOT ARM. ARM/DISARM LEVER BINDS IN ARM POSITION, WILL NOT STAY ARMED. OPS CHECKED THE DOOR ARM LEVER, DETERMINED THAT SLIDE PACK IS RESTING ON THE GIRT BAR CAUSING ARMING LEVER TO MOVE UP. REPLACED THE SLIDE IAW AMM 25-62-44, OPS CHECKED GOOD. SLIDE ARMS AND DISARMS OK.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 77,088 hrs · 29,681 cycles

R1 DOOR ARMS INTERMITTENTLY, REMOVED THE SLIDE, REPOSITIONED THE GIRT BAR TO ALLEVIATE BINDING, REINSTALLED THE SLIDE IAW AMM 25-62-44-000-804-A, AND 25-62- 44-400-803-A.

Part: PLATE — DIRTY (R1 DOOR) · airframe 77,052 hrs · 29,663 cycles

SLIDE DIFFICULT TO ARM AT DOOR 1R FOUND DEBRIS IN THRESHOLD PLATES, CLEANED AND LUBED AND FOUND OPERATION NORMAL.

Part: BATTERY PACK — FAILED (CABIN) · airframe 75,738 hrs · 29,076 cycles

LT FWD EMER LIGHT BATT PACK FAILS CAP CHECK. REPLACED LT FWD EMER LIGHT BATTERY PACK PER AMM 33-51-38-400-002 -A. OPS CHECK GOOD.

Part: BATTERY PACK — FAILED (CABIN) · airframe 75,738 hrs · 29,076 cycles

AFT LT EMER LIGHT BATTERY PACK FAILS CAP CHECK. REMOVED AND REPLACED AFT LT EMER LIGHT BATTERY PACK. OPS CHECK GOOD. REF 33-51-38-400-002-A.

Part: BATTERY PACK — FAILED (CABIN) · airframe 75,738 hrs · 29,076 cycles

LT EMER LIGHT BATTERY PACK FAILS CAP CHECK. REMOVED AND REPLACED LT EMER LIGHT BATTERY PACK, OPS CHECK GOOD REF 33-51-38-400-002-A.

Part: BATTERY PACK — FAILED (CABIN) · airframe 75,738 hrs · 29,076 cycles

RT EMER EXIT BATTERY PACK FAILS CAP CHECK. REPLACED RT EMER EXIT BATTERY PACK PER AMM 33-51-38-400-002-A. OPS CHECK GOOD.

Part: COVER — LOOSE (R2 DOOR) · airframe 74,908 hrs · 28,717 cycles

DOOR 2R SLIDE COVER OFF FOUND BUSTLE LOOSE SECURED SAME.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 73,822 hrs · 28,231 cycles

EMERGENCY LIGHT TEST SHOWS EPSU EMERGENCY LIGHT FAULT. REPLACED EMERGENCY LEFT POWER SUPPLY AND BATTERY IAW MM 33-51-38 PG.0401. EMERGENCY LIGHT TEST OPS CHECKED NORMAL. REPLACED EMERGENCY LEFT EPSU AND BATTERY IAW MM 33-51-38, PG401.

Part: STIFFENER — DAMAGED (FRAME 68) · airframe 73,711 hrs · 28,185 cycles

AFT OF FRAME 68 AT STRINGER 23R HAS A ENONGATED HOLE IN FRAME STIFFNER. REMOVED AND REPLACED THE STIFFENER IAW SRM 53-11-13 FIG 11 AND 51-42-11.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,711 hrs · 28,185 cycles

FWD CARGO STR42R CORRODED 8" FWD OF FR34. STR 42R BETWEEN FR33-34 REPAIRED IAW SRM53-21-13 PARA 5D FG204.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,711 hrs · 28,185 cycles

FWD CARGO UNDER FLOOR BILGE AREA CLEAT ON FR29 AND STR 42R HAS CORROSION ON THE SURFACE. REMOVED AND REPLACED CLEAT IAW SRM 51-72-11.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,711 hrs · 28,185 cycles

AFT FACE OF FR66 HAS CORROSION JUST ABOVE R2 DOOR SILL BEAM. BLENDED AFT FACE OF FR66 JUST ABOVE DOOR SILL BEAM AND FOUND TO BE OUT OF LIMITS ACP NDT OF HOLES AND SURFACE AREA IAW NTM 51-10-08 & 51-10-04 & NO DEFECTS FOUND. FABBED FR66 REPAIR FROM 7075-T7 .098 THICK AND INSTALLED IAW A320 SRM51-42-12 PARA 5A FIG 201 PRINCIPLE I.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,711 hrs · 28,185 cycles

FWD CARGO FR33 STR42R CLEAT HAS CORROSION. REMOVED AND REPLACED CLEAT AT STR 42R FR29 IAW SRM 51-72-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,711 hrs · 28,185 cycles

RT DOOR SILL HAS CORROSION IN FWD GIRT BAR AREA AT FR66. REPLACED R2 DOOR SILL IAW SRM 51-42-11.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,711 hrs · 28,185 cycles

FWD BILGE AREA HAS CORROSION ON CLEAT BETWEEN STR-41L AND STR-40L AT FRAME 34. REMOVED AND REPLACED CLEAT BETWEEN STR41L AND STR40L AT FR 34 IAW SRM 51-72-11.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,711 hrs · 28,185 cycles

FWD CARGO BILGE CLEAT AT STR 43R AND FR32 HAS CORROSION. REPLACED CLEAT AT STR 43R AND FR32 IAW SRM51-42-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,711 hrs · 28,185 cycles

L2 DR SILL HAS CORROSION NEAR FWD GIRT BAR FITTING. L2 DOOR SILL REPAIRED IAW SRM 53-41-14 PARA 5A FG201.

Part: STRINGER — CORRODED (FRAMES 56-57) · corrosion level 2 · airframe 73,711 hrs · 28,185 cycles

AFT CARGO INTERIOR BILGE AREA, STRINGER 42L HAS SURFACE CORROSION BETWEEN FRAMES 56-57. REMOVED AND REPLACED THE STRINGER IAW SRM 51-72-11.

Part: STRINGER — CORRODED (FRAMES 30-31) · corrosion level 2 · airframe 73,711 hrs · 28,185 cycles

FWD CARGO UNDER FLOOR BILGE AREA REPAIR SPLICE ON STR41 R BETWEEN FR30-31 HAS SURFACE CORROSION. REMOVED AND REPLACED SPLICE ON STR 41R BETWEEN FR30-31 FWD CARGO UNDER FLOOR BILGE AREA IAW A320 SRM 51-72-11 PARA 5.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,711 hrs · 28,185 cycles

FWD CARGO CLEAT AT FR27 AND STR 43R HAS CORROSION. REMOVED AND REPLACED CLEAT AT FR27 AT STR 43R IAW SRM 51-72-11.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 72,939 hrs · 27,829 cycles

NUMEROUS CIDS PA LIGHTS INTERMITTENT. CABIN LIGHTS TO FULL BRIGHT ON T/O. BITE CHECK OF CIDS SYSTEM AND OPS CHECKS OF LIGHTS ALL CHECK GOOD. OK TO CONT.

Part: DIRECTOR — FAULTY (CIDS) · airframe 72,906 hrs · 27,812 cycles

ON CLIMB, CONTINUOUS EVAC HORN, AND CI DS 1 & 2 FAULTS ON ECAM. REPLACED 1 & 2 CIDS DIRECTORS REF AMM 23-73-34-400, NO FAULTS AT THIS TIME.

Part: DIRECTOR — FAULTY (CIDS) · airframe 71,504 hrs · 27,205 cycles

EVAC ALARM, CANT SILENCE. REPLACED NR 2 CIDS DIRECTOR IAW AMM 23-73-34-400-001-A. BITE TEST OK IAW AMM 23-73-00-740-003.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,549 hrs · 26,383 cycles

FORWARD LT & AFT LT EMER LIGHT BATTERIES FAIL CAPACITY TEST. REPLACED 10WL & 13WL BATTERIES IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A. CAPACITY TESTED OK IAW AMM 33-51-00-710-003.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 69,108 hrs · 26,191 cycles

INTERIOR LOADS EMER R FAULT WHEN PERFORMING EMER LIGHTS TEST. REMOVED & INSTALLED SAME BATTERY PACK & RESEATED CONNECTOR ON POWER SUPPLY UNIT. RETESTED & CHECKED OKAY.

Part: SKIN — DAMAGED (LT WING) · airframe 69,019 hrs · 26,152 cycles

LEFT WING LOWER SURFACE OPENING FOR FUEL PANEL 540JB HAS ELONGATED SCREW HOLE. REPAIRED HOLE IAW ECRA 5720-02637. REQUIRES 1ST INSPECTION AFTER ACFT 1ST FLIGHT AT 31.1K FC 54.6K FH & SUBSEQUENT INSPECTIONS A T 3.6K FC 4.5K FH IAW SRI 57-21-11 TBL 203. CURRENT PTC 26152 PT T 69019.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,019 hrs · 26,152 cycles

AFT PAX DOOR CUT OUT, DOOR STOP FITTING HOLES AT FRAME 68 WEB, RT POSITION 7 LOWER INBD HOLE IS CRACKED AT APPROX 6 O'CLOCK & 12 O'CLOCK POSITIONS. HOLE WAS OPENED UP TO .417 & CRACK FREE VIA NTM51 -10-01-PB6. FINAL REAM TO .438 & FREEZE PLUG INSTALLED IAW SRM 53-41-12 PG 223 FIG 204 SH 1.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,019 hrs · 26,152 cycles

AFT PAX DOOR CUT OUT, DOOR STOP FITTING HOLES AT FRAME 68 WEB RT POSITION 7 LOWER INBD HOLE IS CRACKED AT APPROX 6 O'CLOCK & 12 O'CLOCK POSITIONS. HOLE WAS OPENED UP TO .417 & CRACK FREE VIA NTM51-10-01-PB6. FINAL REAM TO .438 & FREEZE PLUG INSTALLED IAW SRM 53-41-12 PG 223 FIG 204 SH 1. THIS SRM REFERS TO SRI 53-41-12-2-004-00 PARA 3D TABLE 207 TO INSPECT EVERY 7200C OR 14400T FROM REPAIR EMBODIMENT. THIS REPAIR AT R2 DOOR FRAME 68 STOP 7 LOWER INBD HOLE.

Part: SKIN — DAMAGED (LT WING) · airframe 69,019 hrs · 26,152 cycles

LEFT WING LOWER SURFACE OPENING FOR FUEL PANEL 540JB HAS ELONGATED SCREW HOLE. REPAIRED HOLE IAW ECRA 5720-02637.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,188 hrs · 24,633 cycles

UPPER FUSELAGE SKIN FRAME 60 STRINGER 2L - 3L HAS EXISTING EXT REPAIR IN AREA OF WIFI DOUBLER INSTALLATION. INT SKIN IN SAME AREA HAS EXISTING SCRIBE MARKS AROUND SHEAR TIES & DRILL START. REPLACED EXISTING DOUBLER IAW ECRA 5340-01571 & REO-L01421. BLENDED MINOR SCRIBE MARKS & DRILL START IAW SRM 51-73-00 PG 3. NEGLIGIBLE DMG WITHIN DWG TOLERANCES IAW SKIN DWG D534-70401. NEW APPROVAL MUST BE RECEIVED PRIOR TO 11-27-14.

Part: COVER — UNSECURE (L1 DOOR) · airframe 66,945 hrs · 25,315 cycles

SLIDE PACK AT DOOR 1L IS PREVENTING THE DOOR FROM BEING CLOSED. SECURED DOOR 1L DECORATIVE COVER IAW AMM 25-62-44-000-012-A.

Part: WIRE — DAMAGED (CABIN) · airframe 66,274 hrs · 25,059 cycles

REF 2 SVC EMERGENCY LIGHTS OPERATIONAL TEST MSG DISPLAYED WHEN TEST FAILED. ATA 33-51-38 EXT LOADS FWD L. TESTED AT EPSU, STILL FAILED. ALSO FAILED WITH TESTER CONNECTED AT EACH FWD SLIDE. RANG WIRING FROM 2871VC ON DOOR 1L TO GND & NO GND FOUND. BETWEEN 2871VC A & EPSU T ARE OK. 2870VC A TO EPSU F & B TO GND ARE OK. WIRE REPAIR ACP OF WIRE 3351-5109 IN FWD LT ENTRY DOOR HINGE AREA, SPLICE WIRE IAW ESPM 20-53-21 IAW AWM 33-51-04 BETWEEN 2819VC & 2871VC, OPERATIONS CHECKED GOOD.

Part: FASTENER — LOOSE (FUSELAGE) · airframe 65,403 hrs · 24,714 cycles

TWO FASTENERS LOOSE UNDERBELLY FWD OF RT PACK INLET DOOR. TIGHTENED TWO FASTENERS UNDER BELLY FWD OF RT PACK INLET DOOR.

Part: SOLENOID — FAULTY (APU) · airframe 65,201 hrs · 24,641 cycles

APU WILL NOT START HANGS AT 17% THEN AUTO SHUTS DOWN. AHM ASD RPT 14 INDICATES NO FLAME. HOWEVER DATA ALSO INDICATES POSSIBLE COLD SOAK, EGT NEVER GOT ABOVE -8C, OIL SUMP TEMP -18C & LCIT -16C. DRILL DOWN MCDU TO APU FAULTS CONDITION PG & NOTE LRU ID & TROUBLE SHOT IAW FCN INDICATED. DE-OIL VLV PCN 225-0092, LCIT SNSR 225-0076. REPLACED DE-OILING SOLENOID & INLET PRESS TEMP SENSOR IAW 49-91-49-400-002 & 49-23-17-400-001, OPERATIONS CHECKED APU, OKAY.

Part: TABLE — BINDS (COCKPIT) · airframe 65,096 hrs · 24,597 cycles

FIRST OFFICER'S FLIGHT DECK TABLE IS BINDING. NEEDS ADJUSTMENT WHEN IN THE FULL OPEN SETTING, IT WOBBLES UP & DOWN. REPLACED ROLL PIN, OPERATIONS CHECKED GOOD.

Part: FUSE — FAULTY (BCL 2) · airframe 65,019 hrs · 24,567 cycles

BCL 2 FAULT DISPLAYED ON UPPER ECAM SCREEN, ELECTRICAL. REPLACED FUSE 4PB2 IAW WD24-38-01. CHECKED NORMAL IAW 24-38-00-710-001.

Part: COVER — MISSING (CABIN) · airframe 64,528 hrs · 24,379 cycles

EMERGENCY LIGHTS BUTTON ON AFT FLIGHT ATTENDANT PANEL MISSING CLEAR PROTECTIVE COVER. COMPLIED WITH MEL 2373AU.

Part: SWITCH — INTERMITTENT (COCKPIT) · airframe 64,528 hrs · 24,379 cycles

FIRST OFFICER`S MIC SWITCH ON SIDE STICK STILL INTERMITTENT. FIRST OFFICER`S SIDESTICK TRIGGER SWITCH ARE CAPPED & STOWED.

Part: COVER — MISSING (CABIN) · airframe 64,528 hrs · 24,379 cycles

EMERGENCY LIGHTS BUTTON ON AFT FLIGHT ATTENDANT PANEL MISSING CLEAR PROTECTIVE COVER. IAW MEL 2373AU.

Part: UPLOCK — MALFUNCTIONED (LANDING GEAR) · airframe 64,423 hrs · 24,339 cycles

LANDING GEAR RETRACT, RETURN TO FIELD. REPLACE RT UPLOCK.

Part: INDICATOR — FAILED · airframe 64,416 hrs · 24,334 cycles

EIS 2 WOULD NOT TEST. REPLACED CFDIU REF AMM 31-32-34. MR31333-71 "ON" SN C12860007285 "OFF" REF TSM 31-32-00 MX MESSAGE NO DMC 2 DATA STILL PRESENT. FOUND NO CONTINUITY BETWEEN CFDIU AB 6F AND DMC2 AB 1C. REPAIRED WIRE 3132-7386 AND REINSTALLED ORIGINAL CFDIU DUE TO COA 408131 & REF WDM 31-32-47. REINSTALLED DMC 2 AND BITE TESTED GOOD. ALL UNITS TESTED GOOD REF AMM 31-63-34-400-001A, 31-32-34-400-001A, 31-32-00-740-002A AND EIS INPUT TEST TASKCARD 4R3185011.

Part: WIRE — MISREPAIRED (HYD PUMP) · airframe 64,416 hrs · 24,334 cycles

ELECTRIC HYD PUMP WIRES ARE TERMINATED WITH BLACK ELECTRIC TAPE AND CARGO TAPE. REMOVED BLACK TAPE. LUGS ARE INTACT ON WIRES. SECURED WIRES TO C-B 3802GX, REF W-D 29-24-01. YELLOW PUMP TEST GOOD BY EXTENDING CARGO DOOR ON GROUND POWER ONLY.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 63,821 hrs · 24,094 cycles

LOST E-WD AND F/O SCREENS. LOST BRAKE, SYS 2. FOUND THAT CB "BUS 2-204XP SPLY"(50A), LOCATION: AB2 AT 123VU PANEL HAD TRIPPED, RESET AND ALL AFFECTED SYS INCLUDING THE F/O'S PFD & ND PLUS THE LWR ECAM SCREENS RETURNED TO NORMAL. RAN BOTH ENGINES FOR 10 MINUTES AND TRANSFER POWER FROM BUS 1, BUS 2 AND APU GENERATORS, FOUND CONDITION NORMAL, REF JRH 2-40-5, 2-40-1.

Part: HINGE PIN — MISSING (OXYGEN MASK BOX) · airframe 63,576 hrs · 24,004 cycles

OXYGEN MASK DOOR ON FIRST OFFICER`S SIDE IS DAMAGED. FOUND OXYGEN MASK COMPARTMENT COVER MISSING HINGE PIN AT LEFT UPPER CORNER. REPLACED PIN.

Part: BULLNOSE — DENTED (NR 3 SLAT) · airframe 63,561 hrs · 23,996 cycles

RAMP REPORTED DENT IN LEFT BULLNOSE OF NR 3 SLAT. ACCOMPLISHED PERMANENT REPAIR IAW SRM.

Part: SWITCH — FAULTY (COCKPIT) · airframe 63,480 hrs · 23,967 cycles

CREW REPORT: F/O COMM-MIC TRIGGER INTERMITTENT. CUTS OUT. COMM PANEL MIC SWITCH OK. DEACTIVATED F/O SS PTT SWITCH. DF STICKER APPLIED.

Part: CONTROL UNIT — FAULTY (NR 1) · airframe 63,454 hrs · 23,958 cycles

RIGHT TRANSFER VALVE OPEN DISPLAYED ON UPPER ECAM SCREEN. LEFT AND RIGHT TRANSFER VALVES OPENED AS EXPECTED BUT WERE ACCOMPANIED BY ECAM MESSAGES. LEFT TRANSFER VALVE OPEN DISPLAYED ON UPPER ECAM SCREEN. REFUELING PANEL BATTERY POWER SWITCH MUST NOT BE SET TO THE ONE POSITION.

Part: SDAC — INTERMITTENT (LT OVERWING) · airframe 63,433 hrs · 23,948 cycles

OVERWING SLIDE INDICATION IS INTERMITTENT. VERIFIED LT OVERWING SLIDE IS ARMED. REMOVED AND REPLACED OF NR 1 SDAC, OVERWING SLIDE INDICATION OPS CHECKED GOOD.

Part: SEAT — LOOSE (ROW 32 DEF) · airframe 63,375 hrs · 23,928 cycles

SEAT ROW 32 DEF LOOSE IN SEAT TRACK. SECURED SEAT ASSY, OPS CHECKED GOOD. VERIFIED SEAT PITCH AND SECURITY.

Part: VALVE — LEAKING (CARGO BAY) · airframe 62,773 hrs · 23,694 cycles

AFT CARGO HEAT ECAM MESSAGE DISPLAYED. REPLACED AFT CARGO HEATING PRESSURE REGULATING VALVE PER AMM. LEAK AND OPS CHECKED GOOD.

Part: BRACKET — DAMAGED (EXTINGUISHER) · airframe 62,688 hrs · 23,657 cycles

HALON EXTINGUISHER IN BACK CABIN HAS DAMAGED BRACKET. REPLACED BRACKET.

Part: BRAKE — WORN (NR 3) · airframe 62,290 hrs · 23,512 cycles

NR 3 BRAKE IS WORN TO ULTIMATE LIMIT AND NEEDS TO BE REPLACED. RESET NR 3 BRAKE SAFETY VALVE AND FLOW AND BRAKE ACTUATION NOW NORMAL. BRAKE ASSY REPLACED UNDER SEPARATE WRITE UP.

Part: BRAKE SYS — INOPERATIVE (NR 3) · airframe 62,287 hrs · 23,510 cycles

NUMBER 3 BRAKE 60 NUMBER 4 BRAKE 390. ACTUATED RT BRAKE AND WITNESSED PUCK MOVEMENT ATTEMPTED BRAKE BLEED OF NORMAL AND ALTERNATE SYSTEMS AND GOT GOOD FLOW OUT OF GREEN BLEED PORTS NO FLOW OUT OF YELLOW BLEED PORTS RENDERED NR 3 MLG BRAKE YELLOW SYSTEM INOP PER MEL 32080.

Part: SEAT — LOOSE (32D) · airframe 62,060 hrs · 23,421 cycles

SEAT 32D IS LOOSE IN TRACKS. FOUND FLOOR TRACK ATTACH FOOT ON SEAT ASSY WITH WORN STAR FASTENER. REPLACED FASTENER AND SECURED.

Part: START VALVE — FAULTY (NR 2 ENGINE) · airframe 61,968 hrs · 23,385 cycles

NR 2 ENGINE NO STARTER CUTOUT ON START. REPLACED STARTER AND REPLACED START VALVE. ACP ENGINE START AND OP'S CHECKED NORMAL.

Part: CARPET — OUT OF POSITION (CABIN) · airframe 61,933 hrs · 23,372 cycles

DOOR 2L WILL NOT ARM AND APPEARS TO BE JAMMED. FOUND CARPET COVERING GIRT BAR FITTING. REPOSITIONED CARPET AND DOOR ARMED WITH NO FURTHER PROBLEMS.

Part: SLIDING WINDOW — STUCK (COCKPIT) · airframe 61,452 hrs · 23,188 cycles

CAPTAIN'S WINDOW STUCK OPEN. SECURED CAPTAIN'S COCKPIT SLIDING WINDOW CLOSED.

Part: PAINT — PEELING (RADOME) · airframe 61,195 hrs · 23,088 cycles

RADOME PEELING PAINT IS NOT WITHIN LIMITS. ACCOMPLISHED PAINT PER MM 51-75-11.

Part: COUPLING — LEAKING (BLEED AIR) · airframe 61,161 hrs · 23,073 cycles

LT WING LOOP 'A' MESSAGE. FOUND AIR DUCT LEAK AT SLIP COUPLING, REPLACED SEAL.

Part: SLEEVE — DAMAGED (THRUST REVERSER) · airframe 61,155 hrs · 23,070 cycles

INBD BLOCKER DOOR AT 7 O'CLOCK POS ON NR 2 ENGINE HAS TWO BROKEN SUPPORT FITTINGS AND ONE BENT CONTROL ROD. FOUND ON LANDING. REPLACED NR 2 TRANSLATING SLEEVE PER MM.

Part: CONTROLLER — FAULTY (NR 1 A/C PACK) · airframe 61,013 hrs · 23,026 cycles

CFDS TEMP CONTROL TEST IN CDU FAULTS P1 AND P2 CONTROLLERS. REPLACED NR 1 PACK TEMP CONTROLLER (7HH) PER MM. DURING OPS TEST OF CABIN TEMP CONTROLLER, FAILS NR 1 PACK RAM AIR IN ACTUATOR (8HH).

Part: HANDLE — UNSECURE (AFT CARGO DOOR) · airframe 60,787 hrs · 22,934 cycles

AFT CARGO DOOR ECAM ON TAKEOFF ROLL. FOUND AFT CARGO DOOR HANDLE POPPED OUT, CLEANED AND LUBED DOOR HANDLE AND OPS CHECKED OK WITH HANDLE STOWED AND LIGHT CHECKED OK REF MT 52-019.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 60,628 hrs · 22,873 cycles

ON NR 3 SERVICE DOOR, EMERGENCY LIGHT CHECK, FAILED FWD LEFT BATTERY PACK. REPLACED FWD LEFT BATTERY PACK PER MM, OPS CHECKED GOOD.

Part: GIRT BAR — OUT OF ADJUST (L2 DOOR) · airframe 60,105 hrs · 22,682 cycles

DOOR 2L WILL NOT INDICATE ARMED. ADJUSTED GIRT BAR, OPS CHECK OKAY.

Part: WIRE — BROKEN (EVAC SLIDE) · airframe 59,885 hrs · 22,602 cycles

CABIN - NR 2 RT PAX-CREW DOOR SLIDE- RAFT P/N MR25115-028 ELECTRICAL WIRES ARE BROKEN. FROM BASE WRITE-UP L3760M. (NOTE: WIRES APPEAR TO HAVE BEEN BROKEN WHILE SLIDE RAFT WAS IN STORAGE DURING DOOR MAINTENANCE. REPLACED 2R DOOR SLIDE.

Part: WINDOW — OUT OF TOLERANCE (COCKPIT) · airframe 59,885 hrs · 22,602 cycles

LT FIREX WINDOW DAMAGED. REMOVED AND REPLACED LT FIREX WINDOW.

Part: CONTAINER — NO TEST (OXYGEN MASK) · airframe 59,885 hrs · 22,602 cycles

RT SEAT ROWS NR 1 & 2 - O2 CONTAINER FAILED TO OPERATE DURING MANUAL RELEASE TEST. REPLACED CONTAINER ASSY PER MM. OPS CHECKED GOOD.

Part: CONTAINER — NO TEST (OXYGEN MASKS) · airframe 59,885 hrs · 22,602 cycles

LEFT SEAT ROWS NR 1 & 2 O2 CONTAINERS FAILED TO OPEN DURING MANUAL RELEASE TEST. REPLACED CONTAINER ASSY PER MM, OPS CHECKED GOOD.

Part: EXTINGUISHER — OUT OF TOLERANCE (AFT CABIN) · airframe 57,932 hrs · 21,849 cycles

FIRE EXTINGUISHER IN AFT CABIN MISSING SAFETY WIRE. REPLACED AND SECURED WATER FIRE EXTINGUISHER.

Part: BATTERY — FAULTY (NR 2) · airframe 57,689 hrs · 21,757 cycles

NR 2 SHIP BATTERY IS DRAWING 60 AMPS. REPLACED NR 2 BATTERY & NR 2 BCL PER MM.

Part: FUSE — FAULTY (CONTROLLER) · airframe 57,668 hrs · 21,748 cycles

INTEGRAL LIGHTING OVERHEAD PANEL INOP. LIGHTS CREW COMMENTS: BACKGRND LGTS FOR FUEL AND FIRE PANEL ON OVHD INOP. REPLACED FUSE IN 6LF CONTROLLER. PANEL BACKGROUND LIGHT OP CHECK GOOD.

Part: MOTOR — MALFUNCTIONED (POTABLE WATER) · airframe 57,529 hrs · 21,691 cycles

WATER SYSTEM C-B AT 2001VU POPPING. FOUND DRAIN VALVE 14MP POPPING C-B AND OVERFILL VALVE DRIVING OPEN 8MP. WITH CONNECTOR REMOVED C-B STAYS CLOSED. CONNECTOR REMOVED, CAPED AND TYED BACK. WILL NEED TO BE MANUAL FILL. VALVES LOCATED IN FWD PIT BEHIND RT AFT WALL. NESTING SYS WILL NEED TO BE MOVED FORWARD TO ACCESS PIT WALL. SUSPECT LIMIT SW 3MP DRIVING VALVES OPEN. REPLACED DRAIN VLV MOTOR 14MP. ALSO REPLACE LIMIT SWITCH 3MP AND 5MP DUE TO OVERFLOW VLV STAYING OPEN, OPS CHECKS OKAY. NO LEAKS NOTED. ALSO FOUND DRAIN HANDLE STICKING - LUBED.

Part: UNKNOWN — LEAKING (WASTE DISPOSAL) · airframe 57,471 hrs · 21,666 cycles

FOUL ODOR THROUGHOUT ACFT. FLEW ACFT LAST 2 DAYS. NOTICED POOL OF BLUE WATER FROM SMALL AREA IN REAR PIT.

Part: COUPLING — CORRODED (LAV DUMP) · airframe 57,471 hrs · 21,666 cycles

COUPLING ON LAV TANK DUMP TUBE FOUND CORRODED. EXPANDED BROKEN AND FLUID LEAKING FROM SAME. REPLACED O-RINGS AND COUPLINGS, LEAK CHECKS OKAY.

Part: CONE — CRACKED (NR 2 EXHAUST) · airframe 57,463 hrs · 21,662 cycles

NR 2 ENGINE EXHAUST CONE HAS MULTIPLE CRACKS ON THE FWD END BETWEEN APROX 8 O'CLOCK AND 10 O'CLOCK POSITION AND HAS A 2 1-8" CRACK AT THE AFT END AT 9 O'CLOCK POSITION. REPLACED EXHAUST CONE PER MM. ROBBED EXHAUST CONE FROM ENG 2 ACFT 4238.

Part: BRACKET — BROKEN (VANITY DOOR) · airframe 56,629 hrs · 21,324 cycles

AFT CABIN FWD LAVATORY UNDERSINK VANITY DOOR BROKEN. DOOR HINGE BROKEN AWAY FROM VANITY ASSEMBLY. PART OF FIRE INTERGRITY OF LAVATORY FIRE EXT SYSTEM. LAVATORY NOT USEABLE. INSTALLED NEW BOTTOM BRACKET.

Part: BYPASS SWITCH — LEAKING (OIL SYSTEM) · airframe 56,607 hrs · 21,314 cycles

ABNORMAL ODOR IN COCKPIT AND CABIN DURING CLIMB AND DESCENT. FLT ATTENDANTS REPORTED ODOR CAUSING EYE AND THROAT IRRITATION AND WAS STRONG IN THE CABIN. ACCOMPLISH TROUBLESHOOTING STEPS AS OUTLINED IN MT 72-016. TROUBLESHOOTING TO INCLUDE BORO OF HPC STAGES 3 AND 4. ACCOMPLISHED MT 72-016, FOUND OIL LEAK AT THE OIL FILTER BYPASS SWITCH LEAKING INTO THE APU INLET. INOP APU AND ACCOMPLISHED PNEUMATIC DUCT BURNOUT, CABIN SMELL NORMAL.

Part: ACCUMULATOR — OVERSERVICED (L1 DOOR) · airframe 56,485 hrs · 21,264 cycles

DOOR 1L SLIDE ARMING LEVER IS STIFF DIFFICULT TO ARM. FOUND DOOR DAMPNER ACCUMULATOR OVERSERVICED. SERVICED TO CORRECT PRESSURE IAW AMM.

Part: LINKAGE — LOOSE (L1 DOOR) · airframe 56,011 hrs · 21,075 cycles

DOOR 1L DIFFICULT TO CLOSE. DOOR L/E IS .75 TO 1 INCH FROM FAIRED WHILE DOOR T/E IS FLUSH WITH FUSELAGE. PULLING ON DOOR HANDLE FROM INSIDE DID NOT HELP, COULD NOT LOCK DOOR. DOOR WILL CLOSE SOMETIMES BUT NOT AFTER OPENING ALL THE WAY. DOOR PIVOT POINTS AND LINKAGE AT CENTER OF DOOR APPEARS TO HAVE SLOP IN LINKAGE. REPLACED DAMPNER, EMERGENCY OPS CYLINDER IAW MM ON DOOR 1L. OPS CHECKED GOOD.

Part: LIGHT — NO TEST (CABIN) · airframe 55,950 hrs · 21,045 cycles

EMERGENCY LIGHTS CHECK FAILED ON 3 SVC. RESET EMERGENCY LIGHT CB, OPS TEST NORMAL.

Part: MODULE — MALFUNCTIONED (COCKPIT) · airframe 54,420 hrs · 20,423 cycles

ABORTED TAKEOFF 80-100 KNOTS DUE TO F/O AIRSPEED IND MALFUNCTION. REPLACED ADM 19FP2 PER MM. OPS NORMAL.

Part: LANYARD — BROKEN (GIRT BAR) · airframe 54,334 hrs · 20,379 cycles

LEFT SLIDE HAS GIRT BAR LACING BROKEN. REPLACED SLIDE ASSY IAW MM. OPS TEST IAW MM.

Part: LIFE VEST — OUT OF POSITION (CABIN) · airframe 53,886 hrs · 20,173 cycles

LIFE VESTS ARE NOT IN POUCHES IN CABIN. SECURED 10EA LIFE VESTS IN VARIOUS ROWS, MOSTLY 'C' SEATS.

Part: CONTROL CABLE — FAULTY (DOOR 1R) · airframe 52,774 hrs · 19,737 cycles

CREW REPORTS OF DOOR 1R ARMING LEVER FROZEN. REMOVED DOOR 1R LINING. INSPECTED FLEX CONTROL CABLE FOR SLIDE DISARM LEVER. REMOVED CABLE. INSTALL DOOR 1R FLEXIBLE CONTROL ASSY (ARM CABLE). REPLACED FLEXIBLE CONTROL CABLE.

Part: CABLE — FAULTY (DOOR 1R) · airframe 52,774 hrs · 19,737 cycles

CREW REPORTS OF DOOR 1R ARMING LEVER FROZEN. REMOVED DOOR 1R LINING. INSPECTED FLEX CONTROL CABLE FOR SLIDE DISARM LEVER. REMOVED CABLE. DOOR LINERS IN GALLEY AND COCKPIT. CABLE DIMENSIONS: X1=1.859, X2=.687, X3=.828, X4=2.468. BAD CABLE IS ATTACHED TO DOOR 1 RIGHT. INSTALLED FLEX CABLE.

Part: BALLAST — FAULTY (FWD GALLEY) · airframe 51,994 hrs · 19,364 cycles

FWD GALLEY LIGHT WILL NOT GO BRIGHT. RELAMPED, NO HELP. REPLACED BALLAST 9019WL1. LIGHT OP CHECKS OKAY.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 50,543 hrs · 18,751 cycles

DOOR 1L SLIDE PRESSURE GAUGE. REMOVED AND REPLACED SLIDE-RAFT ASSY.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 50,543 hrs · 18,751 cycles

DOOR 1L SLIDE PRESSURE GAUGE. REMOVED AND REPLACED SLIDE-RAFT ASSY.

Part: UNKNOWN — UNKNOWN (NR 2 EPR) · airframe 49,103 hrs · 18,167 cycles

NR 2 ENGINE EPR FAULT. RTFL.

Part: SLIDE — SHORTED (L1 DOOR) · airframe 48,845 hrs · 18,067 cycles

FAILED EMERGENCY LIGHT TEST. *S/D* INTERNAL SHORT/RESISTANCE IN SLIDE 1L. REPLACED SLIDE 1L. OPS CHECKED GOOD.

Part: SIGN — INADEQUATE (CABIN) · airframe 48,429 hrs · 17,920 cycles

EMERGENCY LIGHT WILL NOT PASS TEST AT 1L. FOUND EXIT SIGN AT 1R OVER DOOR VERY DIM. REPLACED SIGN ASSY, OPS CHECKED NORMAL.

Part: LIGHT — FAILED · airframe 48,419 hrs · 17,915 cycles

EMERGENCY LIGHT TEST ON CIDS PANEL FAILED IT'S TEST. FAULTED THE UNIT.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 47,235 hrs · 17,472 cycles

FLIGHT DIVERTED DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. HYDRAULIC LEAK AT PTU. REPLACED PTU AND ALSO FOUND NR 1 EDP LEAKING, REPLACED AS WELL. SERVICED HYDRO FLUID AND PUT GEAR SYSTEM BACK TO NORMAL CONFIG. ALL SYSTEM TEST GOOD.

Part: STRAP — OUT OF POSITION (EVAC SLIDE) · airframe 47,037 hrs · 17,391 cycles

PART OF SLIDE PACK IS HANGING FROM DOOR 1R WHILE THE DOOR IS CLOSED. D RING STRAP WAS OUTSIDE OF PACK ASSY, SECURED THE D RING STRAP, INSP SLIDE. ALL OK.

Part: SLIDE — FAULTY (L2 DOOR) · airframe 46,758 hrs · 17,284 cycles

PER EMER LIGHT CK ON 3SVC, LEFT AFT DOOR SLIDE FAILED TEST. ELECTRICAL FAULT IN SLIDE 2L. REPLACED SLIDE 2L- OPS CHECKED NORMAL.

Part: WIRE — CRUSHED (EMERGENCY LIGHTS) · airframe 45,821 hrs · 16,913 cycles

SEATS 1, 2, 3, 6, 19 FLOOR PROXIMITY LIGHTS INOP. FOUND CRUSHED WIRING AND WEAK BATTERY/EPSU. REPLACED BATTERY AND EPSU AND REPAIRED AND RELAMPED UNITS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 45,812 hrs · 16,910 cycles

EMERGENCY LIGHT LEFT FWD UNIT FAULT. REPLACED FWD LEFT EPSU BATTERY. OPS CHECK GOOD. NO FAULTS RETURNED.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYSTEM) · airframe 45,503 hrs · 16,793 cycles

CREW REPORTS AT 370 HAD YEL HYD ENG PUMP LO PRESS AND PUMP FAULT LIGHT WITH THE PRESSURE DROPPING TO 2100 PSI. PTU THEN CAME ON LINE. ENG PUMP TURNED OFF. 09-07-07 REPLACED EDP, FILTERS.

Part: GIRT BAR — FAULTY (DOOR 2R) · airframe 45,045 hrs · 16,625 cycles

FOUND 2R DOOR DIFFICULT TO ARM.

Part: STRAP — MISROUTED (GIRT BAR) · airframe 44,529 hrs · 16,431 cycles

MED 2R SLIDE ARMING LEVER CAME OUT OF THE ARM POSITION IN FLIGHT (ALSO ECAM SHOWED NOT ARMED). PER SAMC CYCLED ARMING LEVER AND HANDLE WILL NOT ARM AND SLIGHT NOISE IN DOOR AREA. [06-12-07] FOUND GIRT BAR YELLOW STRAP WEDGED IN GIRT BAR MOUNT SLOT. ROUTED STRAP CORRECTLY.

Part: COVER — OUT OF POSITION (EVAC SLIDE) · airframe 44,235 hrs · 16,315 cycles

THE 2L SLIDE COVER FELL OFF. [SUP 05-18-07] SECURED SLIDE COVER.

Part: PROXIMITY SWITCH — FAULTY (DOOR) · airframe 43,862 hrs · 16,170 cycles

DOOR 1 ARMS, BUT WILL NOT INDICATE ARMED ON COCKPIT. [SUP 05-08-07] FAULT TRACED TO OUT OF ADJUSTMENT PROXIMITY SWITCH. MORE SPECIFICALLY, A LOOSE LOCK WASHER ON THE PROXIMITY TARGET. REPLACED LOCK WASHER AND READJUSTED PROXIMITY SWITCH TO PROPER CLEARANCE.

Part: WIRE — FAULTY (EMERGENCY LIGHTS) · airframe 43,860 hrs · 16,168 cycles

FOUND EMERGENCY EXIT PATH LIGHT IS INOP AT SEAT 18. REPAIRED WIRING UNDER SEAT 18ABC, AT PATH LIGHT CONNECTOR. OPS CHECKED OK.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 43,860 hrs · 16,168 cycles

FOUND EMERGENCY EXIT LIGHTS INOP AT ROWS 1, 2, 3, 6. REPAIR SHORTED WIRES UNDER SEAT 6ABC. ALL EMERGENCY LIGHTS TESTED OK.

Part: RADAR — FAILED · airframe 42,467 hrs · 15,622 cycles

DIVERTED DUE TO LOSS OF RADAR.

Part: STRUCTURE — VIBRATION · airframe 42,024 hrs · 15,443 cycles

FLIGHT REPORTED A VIBRATION ON CLIMBOUT IN THE COCKPIT & A STRONGER VIBRATION IN THE TAIL & AFT GALLEY. ACCOMPLISHED AMM5-50-00. VIBRATION DECICION TREE SUGGESTS TYPE 1 ELEVATOR AS MOST PROBABLE CAUSE. MAINTENACE TIP 53-005 ALSO ACCOMPLISHED. AM27-34-00-200-001 ELEVATOR FREE PLAY CHECK (LT INBD) AND (RT OUTBD) FOUND OUT OF LIMITS. REPLACED LEFT INBOARD ELEVATOR SERVO CONTROLS IN ACCORDANCE WITH AMM27-34-51. REPLACED RIGHT OUTBOARD ELEVATOR SERVO CONTROL IN ACCORDANCE WITH AMM27-34-51. RIGGED BOTH ELEVATOR SERVO CONTROL UNITS PER AMM 27-34-00. WHILE ACCOMPLISHING RT ELEVATOR BUY BACK FURTHER ADJUSTMENT REQUIRED. ACCOMPLISHED ADJUSTMENTS REF AMM27-34-00 OF RT ELEVATOR SERVOS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,908 hrs · 15,396 cycles

EMERGENCY PATH LIGHTING IS INOP AT OVER WING EXT AND ALSO THE EXIT SIGNS ARE INOPERATIVE. REPLACED BATTERY CHARGER GROUND CHECKS NORMAL

Part: BATTERY — FAILED (CABIN) · airframe 41,678 hrs · 15,305 cycles

EMERGENCY LIGHT TEST FAILS. REPLACED BATTERY AT DOOR 1 LEFT. TESTS OK.

Part: CYLINDER — LOW PRESSURE (L2 DOOR SLIDE) · airframe 41,252 hrs · 15,129 cycles

FOUND DOOR 2L SLIDE PACK INFLATION CYLINDER PRESSURE LOW. REPLACED DOOR 2L SLIDE/RAFT. SLIDE/RAFT REMOVED DID NOT FULLY DEPLOY DUE TO A LEAK FROM ONE OF THE SEAMS. FIRST REPLACEMENT SLIDE/RAFT REJECTED DUE TO LOW PRESSURE. SECOND REPLACEMENT INSTALLED.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 38,868 hrs · 14,118 cycles

EMERGENCY LIGHTS BITE TEST FAILS "BATT FWD L". REPLACED FWD LT EMERGENCY BATTERY PACK.

Part: EPSU — MALFUNCTIONED (112WL2-111WL2-11) · airframe 38,830 hrs · 14,108 cycles

EMERGENCY EXIT PATHWAY LIGHTS WILL NOT EXTINGUISH. REPLACED EMERGENCY POWER SUPPLIES 112WL2, 111WL2 AND 110WL2. OPS CHECK GOOD.

Part: LIGHT — WILL NOT TEST (1L DOOR SLIDE) · airframe 38,788 hrs · 14,094 cycles

WHILE PERFORMING EMERGENCY LIGHT TEST FAILED WITH MESSAGE EXT LOADS FWD LEFT. REPLACED SLIDE.

Part: TRANSDUCER — FAILED (GREEN SYSTEM) · airframe 37,930 hrs · 13,803 cycles

CREW RECEIVED LOW PRESSURE GREEN HYDRAULIC PUMP INDICATION. GREEN SYSTEM PRESSURE TRANSDUCER FAILED. REPLACED THE TRANSDUCER.

Part: YAW DAMPER — LEAKING (GREEN HYD SYS) · airframe 34,710 hrs · 12,700 cycles

FLT LANDED UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. YAW DAMPER NR 1 WAS FOUND LEAKING. UNIT WAS REPLACED. OPERATIONS CHECK NORMAL.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 32,678 hrs · 11,990 cycles

RETURN TO FIELD DUE TO INABILITY TO PRESSURIZE AIRCRAFT. REPLACED FAULTY SKIN AIR OUTFLOW VALVE.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 32,471 hrs · 11,911 cycles

WATER INGRESS WAS FOUND AT 2 LOCATIONS ON THE RT ELEVATOR. DAMAGE ON UPPER SKIN IS 2.8 BY 2 INCHES AND IS 127 INCHES FROM IB EDGE AND 20 FROM TRAILING EDGE. MAJOR REPAIR ACCOMPLISHED. REPAIR DAMAGED AREAS PER SRM 55-21-11 TO ELIMINATE WATER INGRESSION.

Part: STRUCTURE — CONTAMINATED (ELEVATOR) · airframe 32,471 hrs · 11,911 cycles

INDICATIONS OF WATER INGRESS WERE FOUND IN 4 AREAS. ALL AREAS WERE APPROX 2.5 X 2 INCHES AND WERE APPROX 3 INCHES FROM THE TRAILING EDGE. THE FIRST AREA WAS ON THE LT UPPER SURFACE 102 INCHES FROM THE INBOARD EDGE. THE OTHER 3 AREAS WERE ON THE LT LOWER SURFACE.

Part: BRAKE ASSY — MALFUNCTIONED (NR 1) · airframe 29,339 hrs · 10,793 cycles

RETURNED TO FIELD UNDER AMBER ALERT DUE TO LEFT BRAKE WOULD NOT COOL. REPLACED NR 1 BRAKE ASSEMBLY. NO PREVIOUS HISTORY OF HIGH TEMPS. NO FURTHER DEFECTS ON SUBSEQUENT FLIGHTS.

Part: LIGHT — WILL NOT TEST (CABIN) · airframe 23,488 hrs · 8,634 cycles

EMERGENCY LIGHTS FAIL TEST FROM THE PROGRAMMING AND TEST PANEL. REPLACED RIGHT HAND OVERWING EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL TEST NORMAL.

Part: LIGHT — INOPERATIVE (ROW 15 - 23) · airframe 22,555 hrs · 8,308 cycles

EMERGENCY ESCAPE LIGHTS AT ROWS 15, 16, 17, 21, 22, 23 NOT OPERATING DURING EMERGENCY LIGHT TEST.

Part: FAN — FAILED (CABIN) · airframe 22,068 hrs · 8,145 cycles

STRONG ODOR THROUGHOUT CABIN IN DESCENT THRU 4000 FT. *S/D* FOUND AVIONICS BLOWER 20HQ TO BE MAKING EXCESSIVE NOISE. REMOVED AND REPLACED FAN. OPERATIONAL CHECK GOOD.

Part: LGCIU — DAMAGED (NR 1)

ECAM FOR UNSAFE LANDING GEAR DISPLAYED. CAPT RECYCLED GEAR AND IT CAME DOWN AND LOCKED NORMALLY. *S/D* CAPT RECYCLED GEAR AND IT CAME DOWN AND LOCKED NORMALLY. REPLACED NR 1 LGCIU DUE TO BROKEN PIN AT J-1. INSPECTED PROX SENSORS 13GA AND 19GA. JACKED AIRCRAFT, SWUNG GEAR SEVERAL TIMES. ALL INDICATIONS NORMAL. NO ECAM MSGS DISPLAYED.

Part: SEAT — CRACKED (CABIN)

DURING THE FIRST HEAVY MAINTENANCE VISIT, VIRTUALLY 100 PERCENT OF THE SEAT PANS ON THE RECARO MODEL 3410, 720 SERIES COACH SEATS WERE FOUND CRACKED AT THE FORWARD EDGE OF THE SEAT PAN. THE CRACKS ARE AT THE MOUNTING HOLES WHERE THE SEAT PAN MOUNTS TO THE SEAT FRAME. THE PAN IS IDENTIFIED BY THE MANUFACTURER OF THE SEAT AS PRIMARY STRUCTURE. A MINIMUM OF ONE CRACK PER SEAT PAN HAS BEEN FOUND WITH THE NORM BEING 2 CRACKS PER PAN. AN AD IS NEEDED FOR REPETITIVE INSPECTIONS OF THESE SEAT PANS TO INSURE THEIR INTEGRITY. NOTE: THERE ARE 132 OF THESE SEAT PANS ON THE AIRCRAFT.

Part: LIGHT — FAILED TEST (CABIN)

EMERGENCY ESCAPE LIGHTS FAIL OPERATIONAL TEST.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

EEL LIGHTS INOP AT DOOR 1L. REPLACED BATTERY PACK.