N818UA

Part: LIGHT — SHORTED (RT WING) · airframe 80,762 hrs · 35,234 cycles

PROCEDURE - EPSU EXT LOAD EMER R FAULT ON PTP AFTER EMER SYS TEST EXTERIOR LIGHT FAULT LIGHT ON RIGHT EPSU (PIC INCLUDED) RIGHT OVER WING EXTERIOR LIGHTS NOT WORKING RELAMPED OVERWING EXTERIOR LIGHTS, NO HELP. NO POWER AT PIN B, REINSTALLED LIGHTS ON FARING T/S REF ASM 33-51-02. FOUND AFT EMERGENCY OVERWING LIGHT 62WL SHORTED. REPLACED REF AMM 33-51-15. OP CHECKS GOOD. MESSAGE CLEARED.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 80,762 hrs · 35,234 cycles

EMERGENCY AISLE LIGHT INOPERATIVE AT ROW 31. R & R EMERGENCY LIGHT ASSY AT ROW 31 IAW AMM 33-51-20. OK FOR SERVICE.

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 80,441 hrs · 35,053 cycles

EPSU EXT LOAD EMER R FAULT. REPLACED 12W EPSU REF AMM 33-51-38-401. OPS CHECKS GOOD.

Part: BLEED VALVE — FAULTED (NR 2 ENGINE) · airframe 80,031 hrs · 34,818 cycles

ENG 2 STALL ON CLIMBOUT. NOTICABLE YAW. ECAM CLEARED ITSELF. NO SHUTDOWNOPENED UP ENGINE NUMBER 2 FOR BOROSCOPE INSPECTION PER TSM 71-00-00-810-809-A STEP D2(A).PLEASE NOTE I ONLY BROKE LOOSE BOROSCOPE PLUGS 3 TO 7 PER THE AMM 72-00-00-200-016-B. BOROSCOPE PLUGS ARE STILL INSTALLED, JUST LOOSE REFER TO PICTURE BELOW FOR REFENENCE OF LOCATION.BOROSCOPE STREAMERS ARE AT THE HANGER AND HAVE BEEN REQUESTED TO BE BROUGHT DOWN TO GATE B16 ASAP. PLEASE NOTE THAT BLEED VALVE AND GASKETS HAVE BEEN ORDERED AND IS CURRENTLY SITTING IN THE LEADS OFFICE IN T1 SENT TO INSP ACP BORO IAW AMM 71-00-00-710-019-B. NO LIMITING FOUND COMPLETED CLOSEUP OF BORESCOPE INSPECTION. REF LPS 4821191, 4822461, 4821212, 4821202, AND 4821221 FOR PLUG INSTALLATIONS. PERFORMED OPS TEST OF FADEC SYSTEM. NO FAULTS FOUND REF MM 73-22-00-710-040-A. PERFORMED DVI OF THE BURNER PRESSURE SENSOR TUBE AND PURGE OF THE BURNER PRESSURE SENSE LINE. REF MM 73-22-49-220-040-A. NO MOISTURE FOUND. NEXT STEP TO PERFORM FUNCTIONAL CHECK OF THE HPC 7TH STAGE 7A AND 7C BLEED VALVES. REF TSM 71-00-00-810-809-A ADD EMP:431164 STEP 4 D (5). R/R 10TH,7B,7A STAGE BLEED VALVE PERFORMED FUNCTIONAL CHECK OF HPC 7TH STAGE BLEED VALVES (AMM 75-32-51-700-010COMPLETED TSM 71-00-00-810-809-A. HIGH POWER ASSURANCE TEST NO 11 REF AMM 71-00-00-710-013-C. OPS CHECK GOOD. NO MATERIAL FOUND. TAT INDICATING WITHIN 1 DEGREE CELCIUS. NOMADDITIONAL FAULTS NOTED. PLANE RETURNED TO NORMAL CONDITION.

Part: DOOR FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 79,888 hrs · 34,736 cycles

R/H FR16 LOWER DOOR CUTOUT PREVIOUS BLEND REPAIR. (REQUEST PERMA NENT REPAIR INSTRUCTIONS AS PER PART OF EC/RA#5311-01839. REPAIRED RH FRAME 16 AFT WEB FACE AT Z-520 IAW ECRA 5311-03353. WORK ACCOMPLISHED ON HAECO N/R 9290354. ACCOMPLISH A PERMANENT REPAIR ON THE RH FR16 AFT WEB FACE AT Z-520 FLOOR LEVEL REINFORCING REPAIR PER PART 3 OF THE LATEST REVISION OF ECRA 5311-03353.

Part: FRAME — CRACKED (ZONE 100) · airframe 79,888 hrs · 34,736 cycles

R/H FR16 DOUBLE JOGGLE HOLE "A" HAS A CRACK INDICATION AT 9 O'CL OCK IN THE FRAME LAYER. REPAIRED HOLE A R/H FRAME 16 DOUBLE JOGGLE WITH BUSHING AND WASH ER IAW SRM 53-11-12-300-012. FINAL HOLE SIZE REAMED WITH BUSING INSTALLED IS .2175. HFEC ACCOMPLISHED WITH NO FINDINGS.

Part: FRAME — CRACKED (ZONE 100) · airframe 79,888 hrs · 34,736 cycles

R/H FR16 DOUBLE JOGGLE HOLE "C" HAS A CRACK INDICATION AT 9 O'CL OCK IN THE FRAME LAYER. REPAIRED HOLE C R/H FRAME 16 DOUBLE JOGGLE WITH BUSHING AND WASH ER IAW SRM 53-11-12-300-012. FINAL HOLE SIZE REAMED WITH BUSING INSTALLED IS .2175. HFEC ACCOMPLISHED WITH NO FINDINGS.

Part: SKIN — CONTAMINATED (ZONE 300) · airframe 79,888 hrs · 34,736 cycles

L/H ELEVATOR HAS LIQUID INGRESS 39.5 IN FROM INBOARD EDGE, 6 IN FROM TRAILING EDGE, 2.5 IN DIAMETER, "REPAIR BEFORE NEXT FLIGHT" PER HAECO LCQ NON ROUTINE 9290380/26380. SEE HAECO NON-ROUTINE 9290380 FOR WORK ACCOMPLISHED. REPAIRED L/H ELEVATOR 39.5 IN FROM I/B 6IN FROM T/E 4.75IN LENGT H 2.25IN WIDTH ZONE C IAW A319 SRM 55-21-11-300-005 CATEGORY A R EPAIR.

Part: SLIDE — OUT OF POSITION (ZONE 800) · airframe 79,346 hrs · 34,466 cycles

DOOR 2L SLIDE PRESSUREGAUGE HAS SHIFTED FORWARD OUT OF VIEW.POS SIBLESLIDE OUT OF POSITION REMOVED DOOR 2L SLIDE REF AMM 25-62-44-000-002-A. UP TO AND INCLUDING STEP 4.A. INSTALLED NEW DOOR SLIDE ASSY AT DOOR 2L REF AMM 25-62-44-400-006-A. RENDER SAFE CHECKLIST ACP. RII INSPECTION IAW GMM 09-25-05 & AMM 25-62-44-400-006-A. NO DEFECTS NOTED.

Part: SKIN — CRACKED (ZONE 600 FLAP) · airframe 78,857 hrs · 34,220 cycles

RT WING I/B FLAP BOTTOM SKIN CRACKED. REPAIRED RT IB FLAP BOTTOM SKIN AND INSTALLED DOUBLER IAW A319 S RM 57-52-00-300-003 A319 SRM 51-77-13-911-020 AND A319 SRM 57-52 -00-300-095 AND UAL EC/RA 5752-02019.

Part: FUEL CAP — MISSING (ZONE 500) · airframe 78,462 hrs · 34,025 cycles

PDA 2 REF LOG PAGE 8920951, THE FUELER REPORTED THE FUEL CAP MISSING. CDL 28A ALREADY APPLIED FOR MISSING LANYARD. THE DEFERRAL LOG PAGE WAS UPDATED TO INCLUDE THE CAP.

Part: SEAL — LEAKING (EMERGENCY EXIT) · airframe 78,304 hrs · 33,949 cycles

CREW REPORTED ABNORMAL WIND NOISE COMING FROM BOTH LEFT EMERGENCY EXITS. PRESSURIZATION NORMAL INSPECTED LH OVERWING FROM OUTSIDE DURING PRESSURIZATION CHECK. FOUND LEAKS FROM TOP RIGHT, TOP LEFT, BOTTOM RIGHT, AND FROM HANDLE. SEE ATTATCHED PICTURES PERFORMED PRESSURIZATION CHECK REF AMM 05-53-00-780-002-A01FOUMD DOOR LEAKING. REMOVED LEFT OVERWING DOOR TO INSPECT SEAL, FOUND SEAL TO BE VERY DRY NO TEARS OR CRACKS NOTED. CLEANED & LUBRICATED SEAL & INSTALLED OVERWING DOOR, PRESSURIZED AIRCRAFT NO LEAKS NOTED. REF AMM 52-21-11-400-001-A

Part: SEAL — CRACKED (THRUST REVERSER) · airframe 74,085 hrs · 31,801 cycles

PDA 2 #1 ENG INBD T-R TO PYLON FLEX SEAL CRACKED & PARTIALLY MISSING .... SECOND FROM AFT IS PARTIALLY MISSING AND THIRD FROM AFT IS CRACKED -- SEE PHOTO APPLIED. PER STEP 3 ISSUE DIP TO INSPECT PER PART 2A EZCH FLIGHT CYCLE AND PERMENANT REPAIR PER PART 3 WITHIN 50 FLIGHT HOURS REF ECRA 5450-02357 . PREFORMED PART 1D OF ECRA FOR SPEED TAPE MISSING SECTION - CATEGORY ''C'' REPAIR. 3 LAYERS OF SPEED TAPE TOMC APPROVES THE 54-DIP FOR THE #1 ENG INBD T-R TO PYLON FLEX TOMC-APPROVAL FROM SC1ELBYC COMMENT SEAL CRACKED & PARTIALLY MISSING. PER THE ECRA 5450-02357 MX COMPLETED INTERIM REPAIR PER PART 1D APPLYING SPEED TAPE TO MISSING SECTION AND CRACKED SEAL AS DIRECTED. REQUIRES INSPECTION EACH FLIGHT PER STEP 3. OF REPAIR 1D AND PERMANENT REPAIR WITHIN 50 FLT HOURS. PHOTO ADDED ITEMS 90 AND 110 AS SHOWN IN FIG 3 OF ECRA 5450-02357 REV-B.

Part: SHEAR PANEL — CORRODED (FRMS 69-70) · airframe 73,541 hrs · 31,530 cycles

AFT CABIN SHEAR PLATE LH SIDE IS CORRODED. PER HAECO LCQ NON-ROU TINE 9294440/44440. REMOVED AND REPLACED NEW SHEAR PLATE ON AFT CABIN L/H SIDE FR69 TO FR70 IAW SRM 51-72-11-911-001 AND TOP COATED FASTENERS I AW A319 SRM 51-23-11-001.

Part: SKIN — CRACKED (FRM 35 S28-31L) · airframe 73,439 hrs · 31,478 cycles

SUPPORT TASK: SURVERYED THE FASTENERS AT LH FR35, BETWEEN STRG 2 8 AND STRG 31, A PREVIOUS REPAIR IS SUSPECTED AS FASTENERS ARE A BOVE NOMINAL SIZE. FR35 STR30 LH HAS 3 CRACK INDICATIONS IN HOLE #2 IN FWD SKIN AND AFT SKIN LAYER @3 AND 9 OCLOCK AS SEEN FROM OUTSIDE PER HAECO LCQ NRS 9294264/9294323 44264/44323 GENERATED BY V061742/V892444. SEE LP 3042782 FOR INSPECTION REQUIEMENTS NO FUTHER ACTION REQUIRED ON THE LP

Part: DOOR SILL — CORRODED (R2 DOOR) · airframe 73,439 hrs · 31,478 cycles

R2 DOOR SILL IS CORRODED. R & R R2 DOOR SILL IAW SRM 51-42-11 AND 51-72-11.

Part: CLEAT — CORRODED (R/H FR27) · airframe 73,439 hrs · 31,478 cycles

FWD CARGO PIT R/H FR27 BETWEEN STRINGERS 41R-42R HAS CORROSION A T CLEAT DOT M093. PER HAECO LCQ NON-ROUTINE 9294244/44244 GENERA TED BY V919150. SPEC: A3NB-53-3-6105. REMOVED AND REPLACED CLEAT FWD CARGO R/H FR27 BETWEEN STRINGERS 41R-42R P/N 5323052620017 P.O 1122488.1 IAW A319 SRM 51-42-11/00 1. RESTORED PROTECTIVE COATINGS IAW A319 SRM 51-23-11/001. DOT R EMOVED PER MECH V9235324 INSP V061704

Part: FLANGE — CRACKED (FRAME 68 STR 22) · airframe 73,439 hrs · 31,478 cycles

SUPPORT TASK: FRAME 68 STR 22 RH FLANGE HAS CRACK ABOVE DOOR STO P BOLT #3 PER HAECO LCQ NON-ROUTINE 9294158/44158 GENERATED BY V 892444

Part: FITTING — CRACKED (FR 68 STR 22 LH) · airframe 73,439 hrs · 31,478 cycles

FRAME 68 STR 22 LH HAS CRACK IND. IN FLANGE AT RADIUS ABOVE DOOR STOP BOLT #3 PER HAECO LCQ NON ROUTINE 9294160/44160 GENERATED BY V892444

Part: CLEAT — CORRODED (R/H FR27) · airframe 73,439 hrs · 31,478 cycles

FWD CARGO PIT R/H FR27 BETWEEN STRINGER 42R-43R HAS CORROSION AT CLEAT (A3NB-53-3-6105) GENERATED BY V919150 AT HAECO LCQ PER NR 9294246 (44246) REMOVED AND REPLACED CLEAT FWD CARGO PIT R/H FR27 BETWEEN STRING ERS 42R-43R WITH P/N 5323039820101 IAW A319 SRM 51-72-11-911-001 . APPLIED PRIMER AND TOPCOAT IAW A319 SRM 51-23-11/001 TO FASTEN ERS. PERFORMED BY V932428 INSP BY V061334

Part: FITTING — CRACKED (FD WINDSHIELD) · airframe 73,439 hrs · 31,478 cycles

FLIGHT DECK WINDSHIELD CONTINUITY FITTINGS LH AND RH HAVE CRACK INDICATIONS "CONTACT ENGINEERING FOR REPAIR INSTRCUTIONS BEFORE NEXT FLIGHT" GENERATED AT HAECO LCQ PER NR 9294615 (44615) BY V8 92444 SUPPORT TASK ACCOMPLISHED A CATEGORY A PERMANENT REPAIR ON THE FLIGHT DECK WI NDSHIELD CONTINUITY FITTINGS LH AND RH PER HAECO REO-L24078 REV IR WITH NO DEVIATIONS AND ECRA 5310-08059 PER MECH V061742 INSP BY V061334

Part: DOOR SILL — CORRODED (DOOR 2L) · airframe 73,439 hrs · 31,478 cycles

L2 DOOR SILL PLATE IS CORRODED. PER HAECO LCQ NON-ROUTINE 929444 1/44441 GENERATED BY V892442 SPEC: A3NB-53-3-6357. REPAIRED (2) DOOR SILL PLATE AT FR68 IAW A319 SRM 53-41-14-300-0 01 FIGURE 001 REPAIRED TOPCOAT IAW SRM 51-75-12-911-002 PERFORME D V928628 INSP BY V061334

Part: FRAME — CRACKED (LH EMER EXIT) · airframe 73,439 hrs · 31,478 cycles

LH EMERGENCY EXIT LH FRAME HAS EVIDENCE OF CRACK PER NR9294643/4 4643 GEN BY V935513 RMVD DAMAGED SEGMENT/FRAME ON LH SIDE OF LH EMERGENCY EXIT AND R EPLACED WITH A NEW FRAME IAW SRM 51-72-11-911-001 BY MECH V07484 6 INSP BY V061334

Part: FRAME — CRACKED (RH EMER EXT) · airframe 73,439 hrs · 31,478 cycles

RH EMERGENCY EXIT LH AND RH FRAME HAS EVIDENCE OF CRACK. PER HAE CO LCQ NR 9294644/ 44644 REMOVED DAMAGED RH & LH FRAMES & REPLACED WITH NEW FRAMES IAW A3 19 SRM 51-72-11-911-001 & 002

Part: PANEL — MISSING (FLAP FRNG) · airframe 72,616 hrs · 31,031 cycles

SMALL 2 INCH ROUND ACCESS PANEL MISSING FROMINBOARD SIDE OF OUTER MOST FLP/TRK FRNG RT SIDE REQUESTING CDL 27A. APPLIED SPEED TAPE TO HOLE. COMPLIED WITH CDL 27AD. ADD EMP:U113818 DISPATCH DESK: 06 NAME: AN DATE: 18-MAY-22- OK TO CDL UPDATED NR WITH PICTURES

Part: SEAL — DAMAGED (LAV ACESS PNL) · airframe 71,933 hrs · 30,699 cycles

RAMP REPORTS FWD LAVATORY RIGHT SHROUD ACCESS PANEL PUSHED IN . SECURED INTERIM AS REQUIRED AND DEFERRED IAW NEF 2522NC, DDP C/W STICKER APPLIED. VARGAS TOMC DEFERRED DIRECTLY BY TOMC SHROUD SEAL IS DAMAGED REPORTED BY RAMP UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V930552 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. CONFIRM DOOR NOT MAC RELATED WORK ORDER 000000003035987 AND PRTR BROKEN, IF NEEDED DEFER SEAL DAMAGED PER NEF 2522NC, SECURED INTERIM AS REQUIRED AND DEFERRED INTERIOR OF SHROUD ACCESS PANEL. VARGAS TOMC IAW NEF 2522NC, DDP C/W STICKER APPLIED. TOMC REQUEST 10 HOURS SHIFT SLOT FOR 3 LAV SEE IPC 25-43-42-55P REPOSITIONED FLAPPER PANEL AND INSTALLED SECURITY SEAL

Part: FAIRING — MISSING (NR 4 FLAP TRACK) · airframe 70,140 hrs · 29,808 cycles

PDA 3 REF LOGPAGE #6550149 4 FLAP TRACK FAIRING PIVOT COVERS WERE FOUND MISSING ON ARRIVAL MEX. LOGPAGE #6550149 DEFERED PER CDL 27AD. IAH AND IAD HAVE BEEN INFORMED AND ARE CHECKING LOCALLY FOR POSSIBLE REMOVAL ISSUES THAT OCCURED AND NOT REINSTALLED.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,964 hrs · 29,204 cycles

A3NB-33-3-6012 MAIN CABIN EMERGENCY LIGHT SYSTEM FAILS EPSU BATTERY FWD L33-51-38. (SDR) REF TO PEMCO/AIRBORNE NR 10261.0031. REMOVED AND REPLACED EPSU BATTERY PACK (10WL) (AERO DESIGN,INC), IAW A319 AMM 33-51-38-000-002-A, 33-51-38-400-002-A. OPERATIONS CHECK GOOD, IAW A319 AMM 33-51-00-710-001-A.

Part: SKIN — DENTED (FRAME 27) · airframe 63,267 hrs · 26,417 cycles

LEFT LOWER FUSELAGE SKIN HAS A DENT AT FRAME 27, BETWEEN STRINGERS 38L - 39L. INSTALLED A REPAIR DOUBLER IAW SRM 53-00-11-300-043, FIG 20145, AND SRI53-00-205-017.

Part: HINGE FITTING — WORN (LT MLG DOOR) · airframe 63,267 hrs · 26,417 cycles

LEFT MLG DOOR HINGE FITTING FORWARD LUG, FORWARD FACE, IS WORN AROUND THE BORE. REMOVED AND REPLACED THE MLG DOOR HINGE FITTING IAW SRM 51-4 2-11-001, PARA 2F, AND 51-44-11-001, TABLES 00108 AND 00116.

Part: SKIN — DENTED (NR 3 SLAT) · airframe 63,267 hrs · 26,417 cycles

RIGHT WING NNR 3 SLAT UPPER L/E SKIN DENTED. REPAIRED THE DENT IAW SRM 57- 40-00-300-108.

Part: HINGE FITTING — WORN (RT MLG DOOR) · airframe 63,267 hrs · 26,417 cycles

RIGHT MLG DOOR HINGE FITTING FORWARD LUG, FORWARD FACE, IS WORN AROUND THE BORE. REMOVED & REPLACED THE RT MLG DOOR HINGE FITTING IAW SRM 51-42 -11, PARA 2.F.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 62,300 hrs · 25,978 cycles

AISLE LIGHT COVER AT ROW 22 MISSING NEVER WAS THERE REPLACED LENS COVER ON EMERGENCY ILLUMINATION LIGHT AT ROW 22 CEILING

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 54,906 hrs · 22,147 cycles

LEFT ELEVATOR HAS 1 TRAPPED WATER INDICATION THE LOWER SKIN 88" FROM INBD END & 4.5" FROM TE 3" DIA. & 7" ON UPPER SKIN 39" FROM INBD END 4.5" FROM TE 2.5" DIA 88" FROM INBD END 6" FROM TE 3.5 X 4" DIA, 94" FROM INBD END 5" FROM TE 2.5 DIA, 101.5" FROM INBD END 5" FROM TE 2" DIA, 123" FROM INBD 4.5" FROM TE 3" DIA, 130" FROM INBD END 5.5" FROM TE 3.5 X 4" DIA, 145.5" FROM INBD 5.5" FROM TE 3" DIA. MOISTURE PRESENT. REPAIRED IAW SRM 55-21-11 PARA 5E FIG 205. SRI 55-21-11-2-002-00 REQUIRES REINSPECT AT 48,000C OR 60,000T AFTER COMPONENT DELIVERY. CURRENT 22,147C, 54906:37T.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 54,906 hrs · 22,147 cycles

RIGHT ELEVATOR UPPER PANEL HAS 5 TRAPPED WATER INDICATIONS 54" FROM INBD END 5" FROM TE 4" DIA, 125" FROM INBD END 5" FROM TE 4" DIA, 168" FROM INBD END 4.5" FROM TE 2.5" DIA, 176" FROM INBD END 4.5" FROM TE 3" DIA, 189" FROM INBD END 4" FROM TE 3 X 3.5" DIA, 201" FROM INBD END 3.5" FROM TE 3" DIA. MOISTURE PRESENT. REPAIRED IAW SRM 55-21-11PARA 5E FIG 205. SRI 55-21-11-2-002-00 TABLE 203 REQUIRES REINSPECTION 48,000C 0R 60,000T AFTER COMPONENT DELIVERY. CURRENT 22,147C & 54,906:37T.

Part: SKIN PANEL — SATURATED (RT ELEVATOR) · airframe 54,906 hrs · 22,147 cycles

RIGHT ELEVATOR LOWER SKIN PANEL HAS 2 TRAPPED WATER INDICATIONS 124" FROM INBD END 5" FROM TE 3 X 4" DIA, 139" FROM INBD END 4.5" FROM TE 3 X 3.5" DIA. MOISTURE PRESENT. REPAIRED IAW SRM 55-21-11 PARA 5E FIG 205. SRI 55-21-11-2-002-00 TABLE 203 REQUIRES REINSPECTION 48,000C 0R 60,000T AFTER COMPONENT DELIVERY. CURRENT 22,147C & 54,906:37T.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,906 hrs · 22,147 cycles

R2 DOOR SILL HAS CORROSION ON AFT INBD FLANGE NUTPLATE HOLE. REPAIRED DOOR SILL AT INBD FLANGE IAW SRM 53-41-14 FIG 201 SHEET 3 REPAIR PRINCIPLE 4.

Part: UNKNOWN — ODOR · airframe 54,731 hrs · 22,065 cycles

DURING FLIGHT, ACFT HAS A SMELL SIMILAR TO PLASTIC MELTING IN OVEN. SEEMS TO WORSEN WITH POWER INCREASE. PERFORMED NR 2 ENG WASH. REPLACED LT & RT RECIRCULATION FILTERS. PERFORMED HIGH POWER ENG RUN TO BURN OUT SMELL IAW JRH-2-40-35. NO ODOR AT THIS TIME.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 52,420 hrs · 21,019 cycles

EMERGENCY LIGHT TEST FAILED ON 2 SERVICE. REPLACED RT OVERWING EPSU WL 12 & LT OVERWING EPSU BATTERY IAW MM33-51-38. ACCOMPLISHED OPERATIONAL TEST OF THE EMERGENCY LIGHTS IAW MM33- 51-00, OPERATIONS CHECKED GOOD.

Part: SCREW — MISSING (FUSELAGE) · airframe 52,028 hrs · 20,860 cycles

CORNER & CORNER 1 SCREWS MISSING AT AFT INBD EDGE OF BELLY PNL JUST AFT OF ROT BCN. PLACED ON DEFERRAL NEEDS NUT PLATE PANEL 192KB INBD SIDE IAW 53-35-00-200-002A. ONLY ONE SCREW REMAINS MISSING WHICH IS INBD CTR, ALL OTHERS REPLACED.

Part: SEALANT — MISSING (THRUST REVERSER) · airframe 51,806 hrs · 20,768 cycles

NR 2 ENG THRUST REVERSER C DUCT SEAL, SEALANT, MISSING ON LT & RT HALF, IAW AMM MT78- 016 FOR DISPOSITION. REPAIRED SEAL ON CNA IAW MT 78-001.

Part: CONNECTOR — CORRODED (RT MLG) · airframe 51,797 hrs · 20,762 cycles

REPEAT LOG ON TAXI OUT, MULTIPLE ECAM MESSAGES RELATED TO RT MLG SENSOR 22GA. PHYSICAL INSPECTION OF SENSOR 22GA ON RT GEAR, NO OBVIOUS DEFECTS IAW PFR MESSAGE 32-31-73, 22GA TARGET POSITION SOURCE LGCIU 2, IAW TSM 32-31-00-810-842-A. MESSAGE DID NOT OCCUR UNTIL AFTER BOTH ENGS WERE RUNNING & INITIAL TAXI. SENSOR 22GA CONNECTOR PLUG DETERIORATED INTERNALLY BY CORROSION. CONNECTOR TO 22GA SENSOR WAS REPLACED & CHECKED OK IAW AMM TK 32-69-00-740-001.

Part: SWITCH — DAMAGED (COCKPIT) · airframe 51,533 hrs · 20,647 cycles

WX RADAR SWITCH DAMAGED. REPLACED PANEL GRD CHECKED GOOD BY LAXMM.

Part: ACTUATOR — LEAKING (THRUST REVERSER) · airframe 50,855 hrs · 20,359 cycles

MAINTENANCE WALKAROUND FOUND HYD FLUID LEAKING FROM NR 1 ENGINE LOWER AFT FAN COWLING. FOUND UPPER OUTBOARD ACTUATOR LEAKING. DEACT ENGINE THRUST REVERSER SYSTEM FOR FLIGHT REF MM. STOWED AND LOCKED, NO LEAKS. FOUND THRUST REVERSER ACTUATOR LEAKING AND CHANGED IT ON LOG009. ACFT OK FOR SERVICE, NO LEAKS FOUND.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,250 hrs · 20,092 cycles

DENT IN FUSELAGE, APPROX 2 FEET AFT OF MAIN ENTRY DOOR 1L.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,250 hrs · 20,092 cycles

DENT FOUND OUT OF LIMITS AT C-CHECK. DENT IS AT FR23 AT STR 23L. REPAIR INSTALLED IAW SRM 53-11-11, FIG 212.

Part: UNKNOWN — MISSING (WINDOW) · airframe 49,708 hrs · 19,864 cycles

2L MISSING PLASTIC FROM ARMING WINDOW. CANNOT FIND IT. REPLACED MISSING WINDOW.

Part: LATCH — FAULTY (COCKPIT DOOR) · airframe 49,591 hrs · 19,822 cycles

COCKPIT DOOR DOES NOT LOCK WITH SWITCH SET TO 'NORM'. TOP LATCH IS NOT LOCKED. CAN MANUALLY PULL IT BACK. NO STRIKE OR FAULT LIGHTS ILLUMINATE. ADJUSTED UPPER COCKPIT DOOR LATCH, OPS GOOD.

Part: BRACKET — MISSING (CRASH AXE) · airframe 49,170 hrs · 19,644 cycles

COCKPIT CRASH AX IS MISSING ONE SADDLE BRACKET. REPLACED MISSING BRACKET.

Part: BLADE — DAMAGED (COMPRESSOR) · airframe 47,541 hrs · 18,936 cycles

NR 2 ENGINE BLADE DAMAGE DUE TO BIRD STRIKE. BEGAN REMOVAL OF FAN BLADE IAW REF AMM. CONTINUE INSTALLATION OF OF FAN BLADES I,A,W REF AMM. NEED TO CON, FROM ITEM-7 THRU END. INSTALLED ENTIRE SET OF BLADES REF, V2500 FAN BLADE DISTRIBUTION PROGRAM FOR WINDOWS 1-2. ENGINE S-N V10772 FINISHED INSTALLATION OF NR 2 ENGINE LP COMPRESSOR BLADES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,332 hrs · 18,838 cycles

DURING EMERGENCY LIGHTS TEST EPSU INT LOAD EMERGENCY LIGHT MSG. AISLE LIGHTS AT SEATS 22A BC & 23ABC INOP. EPSU TEST GIVES UNIT FAULT.

Part: UNKNOWN — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 47,332 hrs · 18,838 cycles

DURING EMERGENCY LIGHT TEST EPSU EXT LOAD EMERGENCY LIGHT MSG. WHEN TESTING 11WL EPSU BOTH INT AND EXT LIGHT FAULT FLASH. TRIED NEW EPSU NO HELP ORIGINAL EPSU IS INSTALLED.

Part: CONTROL UNIT — MALFUNCTIONED (MLG) · airframe 46,932 hrs · 18,677 cycles

LGCIU NR 1 FAULT ON UPPER ECAM. RESET LGCIU SYSTEM 1 GND SUPPLY AND SYSTEM 1 CB. BITE TEST SHOWS NO FAULTS. OK TO CONTINUE.

Part: SLIDE — FAULTY (R1 DOOR) · airframe 46,757 hrs · 18,595 cycles

DURING EMERGENCY LIGHT TEST RECEIVED MESSAGES EPSU INT LOAD EMERGENCY L AND EPSU EXT LOAD EMERGENCY. REPLACED DOOR 1 RIGHT SLIDE PER MM 2562-44 PG 401. OPS OK REMOVED ALL LOCK OUTS AND SAFETY AND SOLD INSTALLATION TO INSPECTION.

Part: SOLENOID — MALFUNCTIONED (NR 2 ENGINE) · airframe 46,732 hrs · 18,585 cycles

NR 2 ENG SURGE, RTFL. FOUND 7TH STAGE BLEED VALVE SOLENOID FAILED TEST. REPLACED 7B SOLENOID REF AMM. RAN NR 2 ENG TO 80% N1 MULTIPLE TIMES WITH NO SURGING OR SHIFTING OF PARAMETERS REF JRH. REPLACED FCU PER MM, CHECKED GOOD.

Part: SEAT BELT — DAMAGED (JUMP SEAT) · airframe 45,260 hrs · 17,959 cycles

FWD LEFT F/A JUMPSEAT SHOULDER HARNESS MISSING ADJUSTMENT TAB. REPLACED INOPERATIVE FWD SEAT BELT HARNESS. CHECKED GOOD.

Part: GALLEY MAT — DAMAGED · airframe 45,214 hrs · 17,940 cycles

AFT GALLEY FLOOR MAT DAMAGED. COMPLETED MOISTURE BARRIER AND MAT INSTALLATION. PER AMM.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 45,123 hrs · 17,907 cycles

CAPTAIN'S O2 MASK MIC INOPERATIVE. REPLACED MASK ASSY.

Part: SLIDE — UNSERVICEABLE (CABIN) · airframe 44,812 hrs · 17,767 cycles

ON WALK AROUND FOUND LEFT OVER WING SLIDE STICKING OUT (NOT FAIRED) APPROX 1-2 INCH. 2 OF THE 3 LOCKING-STOW PINS APPEAR TO BE UNDONE-PULLED THRU. REPLACED SLIDE ASSY.

Part: WIRE — DAMAGED (CABIN) · airframe 44,558 hrs · 17,642 cycles

EEL LIGHT AT SEATS 12C AND 32C INOP. REPAIRED WIRING AT BOTH LIGHT ASSEMBLIES.

Part: SLIDING WINDOW — FAULTY (COCKPIT) · airframe 44,544 hrs · 17,636 cycles

2R WINDOW HEAT ISSUE. FO'S SLIDING WINDOW REMOVED FROM ACFT AND SLIDING WINDOW PANEL REMOVED FROM FRAME. REPLACED FO'S SLIDING WINDOW PANEL AND INSTALLED SLIDING WINDOW PER MM. COMPLETED INSTALLATION PER MM STEP 5A TO COMPLETION.

Part: OXYGEN MASK — FAULTY (COCKPIT) · airframe 44,218 hrs · 17,484 cycles

1ST O/B'S OXYGEN MASK MICROPHONE IS INOPERATIVE. REPLACED O2 MASK AND BOX STOWAGE AT FIRST OFFICER SIDE, TESTS OKAY. O2 MASK REPLACED PER AMM. TEST OKAY.

Part: CONVERTER — FALSE ACTIVATION (WINDSHIELD WIPER) · airframe 41,866 hrs · 16,445 cycles

CAPT'S WINDSHIELD WIPER FAILED AGAIN. ACFT REMOVED FROM CAT II AND CAT III SERVICE. NEEDS WIPER MOTOR. REPLACED WIPER MOTOR. MOTOR WORKED ONCE THEN STOPPED. REPLACED WIPER MOTOR SWITCH, SAME CONDITION. MOTOR WORKED ONCE THEN STOPPED. POSSIBLE WIRING OR GROUND PROBLEM. CKD VOLTAGE FROM CKBKR AND HAD 28VDC CKD VOLTAGE AT SOCKET ON WIPER MOTOR HAD 4 OVDC. NEED FURTHER TROUBLESHOOTING. REPLACED WIPER MOTOR. TESTED IAW MM, OPS CHECKED GOOD. CAPT WIPER CONTROL SWITCH 5DB1 WAS REPLACED PRIOR TO MOTOR CONVERTER CHANGE, NO HELP.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 41,038 hrs · 16,031 cycles

CAPTAIN'S SLIDING WINDOW HEATING INOPERATIVE. CHECKED WINDOW RESISTANCE GOOD. REPLACED WHC1 (2DG1) IAW MM. MESSAGE CLEARED AND BITE TEST GOOD.

Part: STATIC INVERTER — OVERHEATED (COCKPIT) · airframe 40,874 hrs · 15,935 cycles

CREW REPORTED THAT WHEN THEY GOT TO THE ACFT TO DO THEIR PREFLIGHT THE COCKPIT WAS FULL OF SMOKE. STATIC INVERTER APPEARS OVERHEATED, NOISY. REPLACED STATIC INVERTER. TESTED NORMALLY, NO EVIDENCE OF HEAT DAMAGE IN AREA.

Part: BEARING — CORRODED (NR 1 PYLON) · airframe 40,713 hrs · 15,863 cycles

NR 1 PYLON SPIGOT BEARING CORRODED. INSTALLED NEW NR1 PYLON SPIGOT BEARING.

Part: SLEEVE — CRACKED (NR 1 PYLON) · airframe 40,713 hrs · 15,863 cycles

NR1 PYLON FWD ATTACHMENT INBD UPR SLEEVE CRACKED. INSTALLED NEW NR1 PYLON FWD INBD UPR SLEEVE.

Part: SLEEVE — CRACKED (NR 2 PYLON) · airframe 40,713 hrs · 15,863 cycles

RIGHT PYLON OUTBOARD UPPER SLEEVE CRACKED. REMOVED CRACK SLEEVE. INSTALLED NEW NR 2 PYLON FWD OUTBOARD UPPER SLEEVE.

Part: SLEEVE — CRACKED (NR 1 PYLON ATTAC) · airframe 40,713 hrs · 15,863 cycles

NUMBER 1 PYLON AFT ATTACHMENT CENTER FITTING HAS CRACKED SLEEVE. RMV'D CRACK SLEEVE. INSTALLED NEW NR 1 ENG PYLON AFT SHACKLE CENTER PIN ASSY.

Part: SLEEVE — CRACKED (NR 1 PYLON) · airframe 40,713 hrs · 15,863 cycles

NR 1 PYLON AFT ATTACHMENT INBD FITTING SLEEVE CRACKED. REMOVED CRACKED SLEEVE. INSTALLED NEW NR 1 ENG PYLON AFT SHACKLE INBD PIN ASSY.

Part: SLEEVE — CRACKED (NR 2 PYLON) · airframe 40,713 hrs · 15,863 cycles

NR 2 ENG PYLON AFT MOUNT LWR INBD SLEEVE CRACKED. REMOVED CRACKED SLEEVE PIN. INSTALLED NEW NR 2 PYLON AFT SHACKLE LWR INBD SLEEVE PIN.

Part: SLEEVE — CRACKED (NR 1 PYLON) · airframe 40,713 hrs · 15,863 cycles

NR 1 PYLON AFT ATTACHMENT OTBD FITTING SLEEVE CRACKED. REMOVED CRACKED SLEEVE. INSTALLED NEW NR 1 ENG PYLON AFT SHACKLE OTBD PIN ASSY.

Part: BEARING — CORRODED (NR 2 PYLON) · airframe 40,713 hrs · 15,863 cycles

NR2 PYLON SPIGOT BALL JOINT SPHERICAL BEARING HAS PITTING CORROSION. INSTALLED NEW NR 2 PYLON SPIGOT BALL JOINT BEARING.

Part: SLEEVE — CRACKED (NR 2 PYLON) · airframe 40,713 hrs · 15,863 cycles

NR 2 PYLON FWD MOUNT UPPER INBD SHACKLE SLEEVE HAS A CRACK AROUND THE SHANK HEAD AREA. INSTALLED NEW SHACKLE SLEEVE.

Part: SLEEVE — CRACKED (NR 2 PYLON) · airframe 40,713 hrs · 15,863 cycles

NR 2 PYLON FWD MOUNT LWR INBD SHACKLE SLEEVE HAS A CRACK AROUND SHANK HEAD AREA. INSTALLED NEW FWD LWR INBD SLEEVE.

Part: OXYGEN MASK — WEAK (COCKPIT) · airframe 40,611 hrs · 15,812 cycles

F/O O2 MASK VERY WEAK OXYGEN FLOW. REPLACED F/O O2 MASK. OXYGEN BOX CHECKS OK.

Part: FAN — FAILED (POSITION 1) · airframe 39,430 hrs · 15,285 cycles

CONTINUED LOUD HUMMING NOISE IN COCKPIT WITH SUBSEQUENT ELECTRICAL ODOR. AVIONICS EXTRACT FAN FAULT DISPLAYED, NOISE STOPPED. REPLACED AVIONICS EXTRACT FAN. AEVC OPS CHECK NORMAL. NO FAULTS NOTED, ALL ECAM CLEAR. SMOKE ODOR HAS DISSIPATED.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 38,484 hrs · 14,863 cycles

EMERGENCY LIGHTS OUT AT SEATS 15 & 16. FOUND SIDE WALL CONNECTOR APART AND WIRE PULLED OUT. REPLACED WALL TO SEAT HARNESS, OPS CHECK NORMAL. NO DEFECTS NOTED.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 38,284 hrs · 14,769 cycles

MED 1R, DOOR ASSIST BOTTLE PRESSURE BELOW LIMITS. SERVICED AS REQUIRED.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 37,990 hrs · 14,612 cycles

REPLACE NR 1 RT DOOR SLIDE ACCT CONNECTOR LACING CORD IS UNSERVICEABLE. REMOVED & REPLACED NR 1 RT DOOR SLIDE.

Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 37,976 hrs · 14,605 cycles

PACK 1 AND 2 FAULTS, RTFL. REPLACED HPV DUE TO LEAK AND REPAIRED LEAK OF CLOSURE SOLENOID LINE. NEW NR 2 ENG HPSOV WILL NOT CLOSE COMPLETELY. BUTTERFLY VALVE BINDS SO ECAM BLEED SHOWS OPEN POSITION ALL THE TIME. REPLACED VALVE AND FLEXIBLE HOSE. ENG 2 RUN TEST OK, NO FAULT ON PFR.

Part: GIRT BAR — OUT OF RIG (R2 DOOR) · airframe 35,420 hrs · 13,492 cycles

PRESSURE CHECK DOOR 2R FOR LEAKS AND MIGRATION OF SLIDE ARMED HANDLE, ACCOUNT OF SCUFF PLATES REPLACED AND GIRT BAR RIGGED. PRESSURE CHECKED DOOR AT 4 LBS, DOOR ARMED HANDLE GOOD, NO DOOR LEAKS.

Part: WIRE — DAMAGED (CABIN) · airframe 35,420 hrs · 13,492 cycles

CABIN EMERGENCY LIGHTS AT SEAT 10 ABC NOT ILLUMINATING. REPAIRED WIRE, TESTS OKAY.

Part: WIRE — DAMAGED (CABIN) · airframe 35,420 hrs · 13,492 cycles

CABIN EMERGENCY LIGHTS AT SEAT 10 ABC NOT ILLUMINATING. REPAIRED WIRE, TESTS OKAY.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,420 hrs · 13,492 cycles

BEAM 140 CORRODED. REMOVED FLOORBEAM 140. TRANSFERRING FASTENER HOLES TO NEW BEAM. INSTALLING FASTENERS IN NEW BEAM. INSTALLED BEAM 140.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,420 hrs · 13,492 cycles

BEAM 95 CORRODED. REMOVED FLOORBEAM 95. REMOVED BRACKETS AND DRILLED NEW BEAM. ALL BRACKETS AND ATTACH FITTINGS INSTALLED. BEAM INSTALLED, ATTACHMENT COMPLETE AT FRAME 64, NEEDS BOLTS AT FRAME 66 AND 65. COMPLETED INSTALLATION OF BEAM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 35,420 hrs · 13,492 cycles

BEAM 95 CORRODED. REMOVED FLOORBEAM 95. REMOVED BRACKETS AND DRILLED NEW BEAM. ALL BRACKETS AND ATTACH FITTINGS INSTALLED. BEAM INSTALLED, ATTACHMENT COMPLETE AT FRAME 64, NEEDS BOLTS AT FRAME 66 AND 65. COMPLETED INSTALLATION OF BEAM.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 35,420 hrs · 13,492 cycles

EVIDENCE OF CORROSION AROUND FWD GIRT BAR ATTACH FITTING DOOR 2R. INSTALLED CORNER FITTINGS AND GIRT BAR HOOK MOUNT PLATES ON NEW DOOR SILL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,420 hrs · 13,492 cycles

BEAM 95 CORRODED. REMOVED FLOORBEAM 95. REMOVED BRACKETS AND DRILLED NEW BEAM AND READY FOR BRACKET INSTALL. ALL BRACKETS AND ATTACH FITTINGS INSTALLED AND READY FOR INSTALLATION INTO AC. BEAM INSTALLED, ATTACHMENT COMPLETE AT FRAME 64, NEEDS BOLTS AT FRAME 66 AND 65. COMPLETED INSTALLATION OF BEAM. FOUND SERVICEABLE.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 35,420 hrs · 13,492 cycles

CORROSION AROUND NUT PLATE HOLES INBOARD OF AFT GIRT BAR FITTING DOOR 2L. REMOVED CORROSION PER MT 53-025. INSPECTED REPAIR PER MT53- 025. FOUND SERVICEABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,420 hrs · 13,492 cycles

BEAM 80 CORRODED. REMOVED FLOORBEAM 80. TRANSFERRING FASTENER HOLES TO NEW BEAM. INSTALLED BEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,420 hrs · 13,492 cycles

BEAM 175 CORRODED. BEAM OUT & BRACKETS INSTALLED ON NEW ONE. INSTALLED BEAM AND FASTENERS WITH SEALANT. INSPECTED BEAM 175 INSTALLATION AND FOUND SERVICEABLE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 35,420 hrs · 13,492 cycles

CORROSION IN AREA OF PREVIOUS REPAIR BEAM 190. REMOVED CORROSION. INSPECTED REPAIR PER MT53- 025, FOUND SERVICEABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,420 hrs · 13,492 cycles

BEAM 145 CORRODED. REMOVED FLOORBEAM 145. TRANSFERRING FASTENER HOLES TO NEW BEAM. INSTALLING FASTENERS IN NEW BEAM. INSTALLED NEW BEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,420 hrs · 13,492 cycles

BEAM 150 CORRODED. REMOVED FLOORBEAM 150. REMOVED BRACKETS AND DRILLED NEW BEAM AND READY FOR BRACKET INSTALL ON NEW BEAM. INSTALLED BEAM, NEEDS 2 BOLTS AT STA 70, 8 BOLTS AT STA 68. COMPLETED INSTALLATION OF BEAM. INSPECTED FINAL INSTALLATION OF BEAM 150. FOUND SERVICEABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,420 hrs · 13,492 cycles

BEAM 140 CORRODED. REMOVED FLOORBEAM 140. TRANSFERRING FASTENER HOLES TO NEW BEAM. INSTALLING FASTENERS IN NEW BEAM. INSTALLED BEAM.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 35,420 hrs · 13,492 cycles

SHEAR PLATE AFT OF DOOR 2R BETWEEN FRAME 69 AND FRAME 70 CORRODED. REMOVED SHEAR PLATE AFT OF DOOR 2R. REPLACED WITH NEW SHEAR PLATE AFT OF DOOR 2R. INSPECTED THE INSTALLATION OF THE SHEAR PLATE AND FOUND SECURE.

Part: BATTERY — FAULTY (CABIN) · airframe 34,344 hrs · 13,094 cycles

EPSU BATTERY FWD LEFT DISPLAYED AFTER CIDS EMERGENCY LIGHT TEST. REPLACED BATTERY ON 10WL EPSU. OP CHECKS OKAY.

Part: TRANSCEIVER — INTERMITTENT (WEATHER RADAR) · airframe 34,243 hrs · 13,053 cycles

WEATHER RADAR SYSTEM INOP, RTFL. TRANSCEIVER IS INTERMITTENT. REPLACED TRANSCEIVER, OPS CHECK OK.

Part: MOTOR — FAILED (VENT) · airframe 33,777 hrs · 12,884 cycles

VENT BLOWER FAULT DISPLAYED WITH ELECTRICAL ODOR IN COCKPIT, NO SMOKE REPORTED. VENT BLOWER MOTOR FAILURE, BEARING. REPLACED AVX VENT BLOWER FAN MOTOR. OPS CHECKED NORMALLY, NO SMELL.

Part: CONTROL UNIT — MALFUNCTIONED (NLG STEERING) · airframe 32,046 hrs · 12,203 cycles

NOSE WHEEL STEERING PULLS TO THE RIGHT WHEN TILLER AT ZERO. FOUND BSCU FAULTY. REPLACED BSCU, NO REPEATS.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 27,534 hrs · 10,434 cycles

DURING CABIN EMERGENCY LIGHT TEST PTP INDICATED EPSU BATTERY AFT LEFT. REPLACED BATTERY AT 13WL, TESTED OK.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 19,874 hrs · 7,524 cycles

F/O'S WINDSHIELD SHATTERED FL370. FLIGHT DIVERTED. MOISTURE INGRESS IN THE BUSBAR AND SENSOR AREA CAUSED THE ARCING, WHICH CAUSED THE WINDOW TO SHATTER. WINDSHIELD WAS REPLACED.

Part: RUB STRIP — DEBONDED (COMPRESSOR) · airframe 15,477 hrs · 5,813 cycles

DIVERTED DUE TO NR 1 ENGINE COMPRESSOR STALL. COMPRESSOR STALL CAUSED BY HIGH PRESSURE COMPRESSOR (HPC) 6TH STAGE (C6) BLADE DAMAGE WHICH WAS IN TURN CAUSED BY HPC C6 RUBSTRIP COATING DISBONDING. SERVICE BULLETIN 72-0369 IS IN PLACE TO UPGRADE COATING TO AVOID DISBOND. THIS SERVICE BULLETIN IS ACTIVELY ACCOMPLISHED AT ENGINE SHOP VISIT.

Part: FILLET — LOOSE (NR 1 ENG PYLON) · airframe 616 hrs · 2,124 cycles

RETURNED TO SFO AFTER NR 1 ENG COWL FILLET AT TOP PYLON TO COWL SECTION CAME LOOSE.

Part: CONE — CRACKED (NR 2 ENGINE) · airframe 4,509 hrs

NR 2 ENG HAS INLET CONE FAIRING CRACKED AROUND BOLT HOLE. *S/D* THE CAUSE OF THE INLET CONE CRACKING IS VIBRATION OF THE INLET CONE FAIRING AGAINST THE INLET CONE SEATING. THE MANUFACTURER ISSUED SERVICE BULLETIN V2500-ENG-72-0318 WHICH MODIFIED THE FAIRINGS WITH A SEAL TO REDUCE VIBRATION. THIS SERVICE BULLETIN WAS IN PROCESS OF INCORPORATION BY COA R-9039-0/1.

Part: BLADE — FAILED (STAGE 4)

RETURNED TO SFO DUE TO NR 1 ENGINE FAILURE. *S/D* STAGE 4 BLADE FAILED IN FATIGUE IN ROOT ATTACHMENT AREA, LIBERATING AIRFOIL AND PLATFORM AND CAUSING EXTENSIVE DOWNSTREAM DAMAGE. THE MANUFACTURER HAS ISOLATED THE CAUSE TO A VSV SCHEDULE INTRODUCED WITH EEC SOFTWARE CHANGE NR 11. EEC SOFTWARE WILL BE REVISED TO REVERT TO PREVIOUS VSV SCHEDULE. A SERVICE BULLETIN IS EXPECTED IN APRIL OF 2000.

Part: INDICATION — MALFUNCTIONED (LANDING GEAR)

AFTER TAKEOFF, ECAM WARNING: GEAR NOT DOWN. RETURNED TO FIELD. *S/D* ACCOMPLISHED LGCIU1 AND LGCIU2 TEST. NO FAULTS FOUND. REPLACED EEC DUE TO EPR PROBLEMS. TESTED FMGC AND AFS SYSTEM, ALL OK.