N403UA

Part: NONE — CRACKED (LH FR68/ STR22) · airframe 89,419 hrs · 34,741 cycles

LH FR68 STR22 INNER CAP AND WEB FLANGE CRACKED AD 20-22-15-05 PE R NR9298099 / 22099 GEN BY V061632 RPR AT LH FR68 STR22 RPR AREA PER PART 3 OF THE LATEST REV OF 5341-01349 PART 1.2. ECRA 5341-01349 ON OR BEFORE 39,741 TOTAL ACFT FC IAW ECRA ACMP INTERIM REPAIR AT LH FR68 STR22 INNER CAP AND WEB FLANGE IAW ECRA 5341-01349 PART 1.1. REQUIRES DIP TO ACCOMPLISH PERM DIP APPROVED PER ECRA 5341-01349 PART 1 STEP 2 ACCOMPLISH TOMC-APPROVAL FROM SC1ELBYC COMMENT PERMANENT REPAIR AT LH FR68 STR22 REPAIRED AREA PER PART 3 OF THE LATEST REVISION OF ECRA 5341-01349 ON OR BEFORE 39,741 TOTAL AIRCRAFT FLIGHT CYCLES. C/W RII INSP @ HAECO LCQ BY V052031 TOMC APPROVED : QC REVIEWED TOMC APPROVED : QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: NONE — CRACKED (LH FR68/ STR22) · airframe 89,419 hrs · 34,741 cycles

LH FR68 STR22 INNER CAP AND WEB FLANGE CRACKED AD 20-22-15-05 PE R NR9298099 / 22099 GEN BY V061632 RPR AT LH FR68 STR22 RPR AREA PER PART 3 OF THE LATEST REV OF 5341-01349 PART 1.2. ECRA 5341-01349 ON OR BEFORE 39,741 TOTAL ACFT FC IAW ECRA ACMP INTERIM REPAIR AT LH FR68 STR22 INNER CAP AND WEB FLANGE IAW ECRA 5341-01349 PART 1.1. REQUIRES DIP TO ACCOMPLISH PERM DIP APPROVED PER ECRA 5341-01349 PART 1 STEP 2 ACCOMPLISH TOMC-APPROVAL FROM SC1ELBYC COMMENT PERMANENT REPAIR AT LH FR68 STR22 REPAIRED AREA PER PART 3 OF THE LATEST REVISION OF ECRA 5341-01349 ON OR BEFORE 39,741 TOTAL AIRCRAFT FLIGHT CYCLES. C/W RII INSP @ HAECO LCQ BY V052031 TOMC APPROVED : QC REVIEWED TOMC APPROVED : QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: FITTING — CRACKED (DOOR 2L) · airframe 89,419 hrs · 34,741 cycles

L2 DOOR LOWER AFT CORNER FITTING CRACKED FR68L. GENERATED AT HAE CO LCQ PER NR 9298438 (22438) BY V077956 {SUPPORT TASK} REMOVED AND REPLACED L2 DOOR LWR AFT CORNER FITTING IAW A320 SRM 51-42-11/001. ACP BY V061619 INSP BY V940824

Part: CONTROLLER — FAILED (INTERNAL) · airframe 88,967 hrs · 34,528 cycles

CAB PR SYS 1 FAULT CPC 1 FAILED IN LAST LEG REPORT. R&;R CPC 1 PER AMM 21-31-34 AND OPS CHECKED GOOD PER AMM TASK 21-31-00-710-002-A ROTABLE PARTS CHANGE WAS INDICATED - TT # 1991893 SN OFF 1779 CONTROLLER, CAB OFF 31-2130-9-0001 1779 ON 31-2130-9-0001 8608

Part: MANIFOLD — LEAKING (HYD SYSTEM) · airframe 88,034 hrs · 34,097 cycles

*EMERGENCY DECLAERD* ECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - HYD HYD Y RSVR LO LVL PULLED AND COLLARD CIRCUIT BREAKERS ON PANEL 123VU - "Y HYD ELEC PULLED AND COLLARED 2 YELLOW ELECT PUMP C/B PUMP" AND "Y PUMP CONTROL" ON PANEL 121VU. FOUND LEAK AT YELLOW SYSTEM HYD PTU MANIFOLD. REMOVED YELLOW SYSTEM PTU MANIFOLD REF AMM 29-13-15000-001-A. PARTS ON ORDER FOR INSTALLATION. ALL LINES HAVE BEEN CAPED AND OR PLUGGED. INSTALLED NEW PACKINGS ON CHECK VALVE 3094GM. REINSTALLED PTU MANIFOLD IAW AMM 29-13-15-400-001-A. RAN ENGINES, OPS CHECK GOOD ON PTU AND NO LEAKS NOTED IAW AMM 29-23-00-710-004-A

Part: SENSING ELEMENT — FAILED (POS 1) · airframe 87,829 hrs · 33,990 cycles

FUEL IMBALANCE WHILE IN LEVEL FLIGHT FUEL QTY READS 1540/11880/40/8860/1560 WITH FOB 23300. ATTEMPTED TO FOLLOW QRH 120.9 & 120.6 WITH THE CROSS FEED VALVE NO HELP. FUEL IMBALANCE CONTINUED TO INCREASE ON THE LEFT WING. CFR INDICATES LEFT PUMP 2 LO PR MESSAGE. REPORTED BY CREW TOMC SMITH DO NOT HAVE A FLSCU IN STOCK IN ATL NOR SPECIALIZED EQUIPMENT FOR TESTING PER PARAGRAGH 4A OF THE TSM 28-46-00-810-810A. ACCOMPLISHED FUEL TRANSFER PER TSM 28-23-00-810-803-A. NO UPDATED PARTS FOR AC 4703 UPDATED SENSOR PART. UNCOMMANDED TRANSFER NOTED AT THIS TIME. OPERATIONAL CHECK GOOD. THERE WAS A L UNFULL SENSOR 26QJ1 MESSAGE FOUND UPON CHECKING POST FLGHT REPORT AND PERFORMING TSM TASK 28-46-00-810-810A WE ADD ACP''D TSM 28-46-00-810-810-A FOR L UNDERFULL LEVEL SENSOR 3 IDLE RUN WITH NO ABNORMAL FUEL TRANSFER INDICATED, AND POST ENG 26QJ1. PER STEP 4(A)6 - REPLACED FLSCU POS 1 (7QJ) PER AMM RUN POST FLT GOOD, CFDS COMMAND FLSS BITE CHECKS GOOD, NO 28-46-34-000-001 & 28-46-34-400-001-A, FUNCTIONAL TESTS GOOD. FAULTS. SET NEW FLT NUMBER, RESET FADECS, RAN BOTH MOTORS FOR 10 MIN ROTABLE PARTS CHANGE WAS INDICATED - TT # 1071328 SN OFF 3446 IPC REFERENCE # 28-46-34 UNIT, FUEL LEVL OFF 31-2840-9-9001 3446 ON 31-2840-9-9001 1852

Part: NONE — NONE (NLG) · airframe 86,871 hrs · 33,548 cycles

NW STEER FAULT DISPLAYED ON UPPER ECAM SCREEN. - WHEEL BOX. PERFORMED RING OUT PER TSM 32-51-00-810-818-A AND ASM 32-51-01 FOR FAULT 10GG STEERING FDBKSENSORS. FOUND HIGH RESISTANCE BETWEEN PIN F AT CONNECTOR 3GC AND PIN AB 9E AT 10GG. ISOLATED UPPER AND LOWER HARNESS AT 1300VC AND VCA, FAULT IS BETWEEN BSCU AND 1300VC,NEED TO REPLACE VC SIDE OF CONNECTOR AT NOSE GEAR REMOVED AND REPLACED VC SIDE OF CONNECTOR 1300VC PER AWM32-21-02 PAGE 6, PERFORMED BSCU 1 AND 2 TEST, TEST PASSED, VERIFIED STEERING ANGLE INPUT MONITORING ON BSCU 1 AND 2, CHECKS OK PER TSM 32-51-00-810-818-A

Part: ACTUATOR — FAILED (NR 2 ENGINE) · airframe 85,986 hrs · 33,138 cycles

PER CREW, NR 2 ENGINE EXCEEDS EGT. PLANE MADE A GATE RETURN UPDATED AIR RETURN CREW REPORTED EVENT HAPPENED IN FLIGHT BEFORE FLAP RETRACT BELOW POPPING FROM NR 2 ENG. 11,000'' ALT. DEAD HEAD PILOT CAPT SITTING ABOVE WING REPORTED (REPORT AIDS) SHOW TOVL1= 0004 SEC, TOVL2= 0000, TOVL3= 0000 AND EIS1, 2 AND 3 (DMC1, 2, & 3) ALL SHOW EGT2 PEAK AT 639. SO EGT PEAKED AT 639 FOR 04 SECOND. REF TSM 77-00-00-810-818-B PARA. 4.E (1). AND SHEET 2 TRANSIENT OVERTEMP IN AREA "A1" HAPPENED. E2 SN V10162: REF TSM 77-00-00-810-818-B, GAS PATH ADVISORY REF LOG PAGE 6609524. 2.5 BLEED ACTUATOR REPLACED

Part: ACTUATOR — INOPERATIVE (LT PACK OUTLET) · airframe 85,753 hrs · 33,034 cycles

AIR PACK 1+2 FAULTPACK 2 ALREADY DF CAPTAIN REPORTS: AIR PACK 1 FAULT DISPLAYED ON ECAM AT FL350, PACK 1 OUTLET TEMPURATURE INDICATION WAS AMBER BEFORE BEGINNING DESCENT. NO CABIN PRESSURE ISSUES NOTED. F/A REPORTS CABIN TEMP UNSATIFACTORY FOR DURATION OF FLIGHT. PERFORMED CABIN AIR TEMP CONTROL TEST. FAILED WITH MSG P1 RAM AIR OUT ACTUATOR 9HH. REPLACED #1 PACK AIR-OUTLET FLAP ACTUATOR REF: AMM 21-61-52. OPS CHK GOOD. ADD EMP:U349258,U104898 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1993535 SN OFF 2027 ACTUATOR, PACK OFF 31-2163-9-0002 2027 ON 31-2163-9-0002 2194

Part: FAULT MESSAGE — FALSE ACTIVATION (FIRE LOOP) · airframe 84,926 hrs · 32,680 cycles

FIRE LOOP A FAULT DISPLAYED ON UPPER ECAM SCREEN. APU, COMPLIED WITH MEL TOM CQC REV PERFORMED. ACCOMPLISHED FDU APU TEST "TEST OK", NO PREVIOUS, ALL OK.

Part: ANCHOR FITTING — DAMAGED (RT MLG WW) · airframe 84,761 hrs · 32,611 cycles

DURING T/S FOR RT WING WHEEL WELL FUEL LEAK FOUND RUST RESIDUE EXITING FROM BETWEEEN MLG RETRACT/EXTEND ACTUATING CYLINDER ANCHORAGE FITTING AND RT AFT SPAR, REF LP 5024720 AND AB DRAWING A320-57-1089. AWAITING ENGINEERING DISPOSITION, REF ORIGINAL LP 5026239 ON HAECO LCQ, REF 9296034 GENERATED BY MECH N078625 DTA ANALYSIS AND PERMANENT REPAIR INSTRUCTIONS REFERENCE TO LP 5592133 PER ECRA 5726-01089. NO OTHER ACTIONS REQUIRED THIS ITEM RII ACP BY LC-10.

Part: ANCHOR FITTING — CRACKED (RT MLG) · airframe 84,761 hrs · 32,611 cycles

DURING INSP 4 SHEARED FASTENERS FOUND ON RT MLG ANCHORAGE FITTING. REPAIRS ACCOMPLISHED, IAW ECRA 5726-01089 AND REQUIRES DTA ANALYSIS, ACCOMPLISH A PERMANENT REPAIR, PER EC5726-01089 PART 3 ON OR BEFORE JUNE 8 2021. PLANNING TO CONTACT ENGINEERING AFTER APRIL 8 2021, BUT BEFORE MAY 8 2021 FOR THE PERMANENT REPAIR. ACCOMPLISH A PERMANENT REPAIR, PER EC5726-01089 PART 3 ON OR BEFORE JUNE 8, 2021. PLANNING TO CONTACT ENGINEERING AFTER APRIL 8, 2021, BUT BEFORE MAY 8, 2021 FOR THE PERMANENT REPAIR. ALL WORK ACCOMPLISHED ON HAECO NR 9296034 REF LP55687658 AND LP50262 39. OK TO DIP INTERIM REPAIR FOR 4 FASTENERS ON THE MLG GEAR JCK ANCHORAGE FITTING ON THE REAR SPARE ON THE RT WING. AFTER REMOVAL OF THE FITTING, A CRACK WAS FOUND AT ONE LOCATION HOLE 56 IN THE REAR SPAR WEB AND CORROSION WAS FOUND IN 52-55. PERMANENT REPAIRS MUST BE PERFORMED, PER PART 3 OF ECRA 5726-01089 ON OR BEFORE JUNE 8, 2021. PLANNING CONTACT ESC AFTER APRIL 8, 2021 BUT BEFORE MAY 8, 2021 TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: FRAME — CRACKED (FRM 43) · airframe 84,761 hrs · 32,611 cycles

RT FRAME FOOT AT FR 43 HOLE HAS A CRACK INDICATION MUST BE REPAIRED BEFORE NEST FLIGHT ON HAECO LCQ, REF 9296378. REMOVED AND REPLACED RM FR 43 AND FOOT FRAME, IAW EC RA NR 5311-0 2477 AND REO-L22808 1R PER NR 9296378.

Part: FRAME — DAMAGED (FRM 16) · airframe 84,761 hrs · 32,611 cycles

8184 REMOVE AND REPLACE FR 16 LT SIDE ON HAECO LCQ, REF 9296133. ACCOMPLISHED FULL REPLACEMENT OF LT SIDE LATERAL FR 16, IAW ECRA 5311-02479 HAECO REO L22773-IR. THIS REPAIR REQUIRES A DIP TO INITIATE A DIP TO ACCOMPLISH INSPECTION REQUIREMENTS OF EC-5311-024 76 FOR HOLE C ON OR BEFORE THE AC REACHES 74311 TOTAL FLIGHT CYCLES.

Part: FRAME — DAMAGED (FRM 16) · airframe 84,761 hrs · 32,611 cycles

INTERIM REPAIR OF FRAME 16 RT HOLE 7 REQUIRING PERMANENT REPAIR OR EG UPDATE OVERDUE. OPBLM CHRISTIANSEN. OPBLM CHRISTIANSEN LOCKED FOR FERRY FLIGHT. TOMC CHRISTIANSEN UNLOCK FOR REPAIR SIGNOFF EG UPDATED ECRA 5311-02440 WITH NEW LIMITS. INSPECTION NOT DUE UNTIL 39,321 CYCLES. CURRENT CYCLES ARE 32,611. ASSIGNMENT WAS BROKEN AND LP 4899140 WAS UPDATED.

Part: SEAL — LEAKING (HYD SYSTEM) · airframe 83,527 hrs · 32,108 cycles

FL270 HYD Y RSVR LO LVL ECAM COMPLETED AND AFTER LANDING NO2 ENG SHUTDOWN. SERVICED YELLOW SYSTEM TO FULL AT ARRIVAL. OPENED GEAR DOORS FOUND HYD FLUID RESIDUE ON AFT BKHD AREA AT PTU DOWN TO KEEL BEAM. OPENED FAN COWL, RAN #2 ENG TO CHECK FOR LEAKAGE AND PRESSURE, OPS NORMAL NO LEAKAGE NOTED, PTU OPS NORMAL CYCLED ALL FLT CONTROLS NO LEAKAGE NOTED. FOUND PTU CASE DRAIN HARD LINE OFF HOSE ASSY AN SOME FLUID DRIPPING. CLEANED AREA. DUE TO CREWS COMMENTS ACCOMPLISHED TASK 32-31-00-790-001-A NO LEAKAGE FOUND IN THOSE SYSTEMS. REMOVED PTU REF AMM 29-23-41-000-001-A NOTE FOUND THE SEAL DRAIN LEAKING ITEM #9 ON SHEET (1) OF AMM. NEW PUMP FROM STOCK REJECTED FROM STOCK. REPLACED PTU DUE TO SEAL FAILURE IN PUMP REF AMM 29-23-41 COMPLETED OPERATIONAL TEST OF PTU. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1057809 SN OFF 0208 IPC REFERENCE # 29-23-41-01 #001G. COMPLETED LEAK CHECK OF PTU AND YELLOW SYSTEM, OPS CHECKED GOOD NO LEAKS AND A HYDRAULIC SYSTEMS SERVICED TO FULL. REF AMM 29-00-99-200-001C1 UNIT, TRANSFER OFF 31-2920-9-0001 0208 ON 31-2920-9-0001 0005.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 82,372 hrs · 31,586 cycles

ECAM CAUTION MESSAGE - Y SYS LO PR MESSAGE INOP - HYD UPON TROUBLESHOOTING FOUND HYD PTU LEAKING AT CHECK VLV AND UNION FOR QUICK DISCONNECT. REPLACED BOTH O-RINGS PER AMM SUBTASK 29-13-15-560-050-E. LEACK CHECK GOOD NO LEAKS FOUND AT THIS TIME & SERVICED YELLOW HYD SYS PER AMM 12-12-29-611-001-A.

Part: STOP FITTING — DAMAGED (FUSELAGE) · airframe 80,399 hrs · 30,740 cycles

L1 DOOR FRAME 16 STOP FITTING NR 1 PRODUCED REJECTABLE INDICATIONS IN THE INBD LOWER BOLT HOLE DURING RHFEC BOLT HOLE INSPECTION REF 9290213 SPEC A3NB-53-4-6304. REAMED DISCREPANT HOLE AT L1 DOOR FR16 STOP FITTING NR 1 AND REPLACED INTERCOSTAL TO REMOVE INDICATION IAW ECRA 5311-02042.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 80,399 hrs · 30,740 cycles

L1 DOOR FRAME 16 STOP FITTING NR 7 PRODUCED REJECTABLE INDICATIONS IN BOTH INBD UPPER & LOWER HOLES DURING RHFEC BOLT HOLE INSPECTION REF 9290208 SPEC A3NBB-53-4-6304. REAMED DISCREPANT HOLE TO 2ND OS AND REPLACED INTERCOSTAL AND REINSTALLED STOP FITTING.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 80,399 hrs · 30,740 cycles

R1 DOOR CUTOUT FR16 DOOR STOP FITTING NR 7 INBD LOWER HOLE HAS A CRACK INDICATION IN INTERCOSTAL AT 8 O''CLOCK POSITION REF 9290332 SPEC A3NB-53-4-6304 AD 2017-22-03. REAMED DISCREPANT HOLE AT R1 DOOR FR 16 STOP FITTING NR 7 TO REMOVE INDICATON IAW ECRA 5311-02042. REMOVED AND REPALCED INTERCOSTAL IAW SRM 51-42-11-001 AND ECRA 5311-02042.

Part: ISOLATION VALVE — FAILED (MLG) · airframe 78,364 hrs · 29,784 cycles

LANDING GEAR DID NOT EXTEND USING GEAR HANDLE. PERFORMED GRAVITY EXTENSION. EMERGENCY DECLARED. IAW TSM 32-31-00-810-808-A. PFR SHOWS RT MLG DOOR ACTUATOR. BOTH LGICUS SHOW NO FAULTS. REPLACED 62GA RELAY AND 49GA LANDING GEAR SYS ISOLATION SAFETY VALVE. REPLACED THE SAFETY VALVE. OPERATED GEAR HANDLE 4 TIMES, DOORS AND GEAR CHECKED OK. NO FAULTS.

Part: ARMING LEVER — MALFUNCTIONED (L2 DOOR) · airframe 78,198 hrs · 29,709 cycles

LEFT AFT SLIDE INDICATION INOPERATIVE ON DOOR, OXYGEN SYSTEM ECAM PAGE, OXYGEN DOOR ARMING HANDLE POPS OUT AND DISARMS. EVEN WHEN ARMED IT DOES NOT LIE FLUSH. CYCLED THE DOOR SEVERAL TIMES WITH NO RESISTANCE ON GROUND. INDICATION NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 77,589 hrs · 29,405 cycles

FWD L EMER LIGHT BATTERY FAULT. REPLACED BATTERY TEST OK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 77,465 hrs · 29,344 cycles

EMERGENCY LIGHT EPSU BATTERY FAULT DURING 2 SERVICE CHECKS. REMOVED AND REPLACED THE BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-51-38-400-002-A

Part: UNKNOWN — SMOKE (NR 1 ENGINE) · airframe 76,404 hrs · 28,868 cycles

PAX REPORTED SMOKE FROM THE NR 1 ENGINE AFTER TAKEOFF. ODOR IN THE CABIN AND NOT IN THE COCKPIT. REMOVED AND REINSTALLED BORO PLUGS AS REQUIRED FOR INSPECTION. NO DEFECTS NOTED. BOROSCOPE CHECKED GOOD IAW AMM 72-00-00.

Part: DOOR SILL — CORRODED (L2 DOORWAY) · corrosion level 2 · airframe 75,300 hrs · 28,395 cycles

CORROSION ON LT DOOR SILL AFT CORNER FITTING AT L2 DOOR. REMOVED & REPLACED IAW SRM 51-42-11.

Part: STRINGER — CORRODED (FRAMES 56-57) · corrosion level 2 · airframe 75,300 hrs · 28,395 cycles

AFT CARGO FRAMES 56-57, STRINGER 44R IS CORRODED. REPAIRED THE STRINGER IAW SRM 53-00-13 FIG 202.

Part: STRINGER — CORRODED (FRAMES 59-60) · corrosion level 2 · airframe 75,300 hrs · 28,395 cycles

AFT CARGO BAY, FRAMES 59-60, STRINGER 43L IS CORRODED. REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SKIN — DENTED (FUSELAGE) · airframe 75,300 hrs · 28,395 cycles

DENT 5 FEET FWD OF L1 DOOR. FOUND TO BE FOUND TO BE OUT OF LIMITS IAW SRM 53-11-11 PAR 4.6. REPAIRED IAW SRM 53-00-11 FIG 240.

Part: SHEAR TIE — CORRODED (FRAME 59) · corrosion level 2 · airframe 75,300 hrs · 28,395 cycles

AFT CARGO BAY FRAME 59 STRINGERS 44-43R SHEAR TIE IS CORRODED REMOVED & REPLACED THE SHEAR TIE IAW SRM 51- 42-11

Part: STRINGER — CORRODED (FRAMES 58-59) · corrosion level 2 · airframe 75,300 hrs · 28,395 cycles

AFT CARGO BAY FRAMES 58-59 STRINGER 41R IS CORRODED REMOVED & REPLACED THE STRINGER IAW SRM 51-72-11.

Part: STRINGER SPLICE — CORRODED (FRAME 31) · corrosion level 2 · airframe 75,300 hrs · 28,395 cycles

FORWARD CARGO STRINGER SPLICE 41L CORRODED JUST FORWARD OF FRAME 31. REMOVED & REPLACED THE STRINGER SPLICE IAW SRM 51-42-11.

Part: STRINGER SPLICE — CORRODED (FRAME 31) · corrosion level 2 · airframe 75,300 hrs · 28,395 cycles

FORWARD CARGO STRINGER SPLICE 43L CORRODED JUST FORWARD OF FRAME 31. REMOVED & REPLACED THE STRINGER SPLICE IAW SRM 51-42-11.

Part: SHEAR TIE — CORRODED (FRAME 32) · corrosion level 2 · airframe 75,300 hrs · 28,395 cycles

FWD CARGO BAY FRAME 32 CLEAT BETWEEN STR.42-43R HAS CORROSION AND ELONGATED. FOUND ELONGATED HOLE ON FWD PIT FRAME 32 CLEAT BETWEEN STR. 42-43R OUT OF LIMITS, REMOVED AND REPLACED CLEAT IAW SRM 51-72-11,51-42-11.

Part: STRINGER — CORRODED (FRAME 31) · corrosion level 2 · airframe 75,300 hrs · 28,395 cycles

FWD CARGO FOUND STRINGER 41L AT AND FWD OF FRAME 31 CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 53-21-13, SRM 51-42-11.

Part: DOOR SILL — CORRODED (L2 DOORWAY) · corrosion level 2 · airframe 75,300 hrs · 28,395 cycles

CORROSION ON L2 DOOR SILL IN NUMEROUS PLACES. REMOVED AND REPLACED L2 DOOR SILL IAW SRM 51-42-11, PG.25, SRM 51-72-11, PG.1

Part: DOOR SILL — CORRODED (R2 DOOR) · corrosion level 2 · airframe 75,300 hrs · 28,395 cycles

R2 DOOR SILL HAS NUMEROUS AREAS OF CORROSION. REMOVED & REPLACED THE DOOR SILL IAW SRM 51-42-11, PG.25 & SRM 51-72-11, PG.1.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,300 hrs · 28,395 cycles

AFT CARGO COMPARTMENT FR 58-59 STRINGER 42L CORRODED. REMOVED & REPLACED STR 42 L FROM FR 53 TO FR 60 IAW SRM 53-00-13, SRM 51-42-11.

Part: WIRE — BROKEN (CABIN) · airframe 72,661 hrs · 27,219 cycles

EMERGENCY ESCAPE PATH FLOOR LIGHT AT SEAT 38 ABC HAS A BROKEN WIRE RUN. REPLACED CONNECTOR. OPERATIONS CHECK OF LIGHT FUNCTION, OPERATION CHECKED NORMAL.

Part: LIGHT — FAILED (ESCAPE SLIDE) · airframe 71,622 hrs · 26,779 cycles

IAW 2 SVC, EMERGENCY LIGHTS FAULT, EXT LOADS AFT L, IS DISPLAYED DURING LIGHTS TEST. REPLACED SLIDE RAFT ASSEMBLY IAW AMM 25-62-44-400-007-A.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 71,069 hrs · 26,561 cycles

EMERGENCY EXIT LIGHTS DID NOT COME ON IN ARM POSITION WHEN GND POWER FAILED. REPLACED LT MID POWER SUPPLY & BATTERY, AFT POWER SUPPLY & BATTERY IAW MM33-51-38-4 01. EMER LIGHTS TESTED OK ON FWD ATTN PANEL & ON EACH POWER PACK. ALL EMER LIGHTS ILLUMINATED IN CABIN WITH POWER OFF IN ARM POSITION.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 70,412 hrs · 26,285 cycles

FRAME 68 AT R2 DOOR LOWER AFT STOP FITTING, INBD LOWER HOLE IS CRACKED AT 6 O’CLOCK. HOLE WAS REPAIRED IAW SRM 53-41-12 PG 222 WITH FREEZE PLUG. THIS IS A CAT B REPAIR & REQUIRES SRI INSPECTION IAW SRM 53-41-12 TABLE 202 ON PAGE 203.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 70,412 hrs · 26,285 cycles

FRAME 66 AT R2 DOOR, 3RD STOP FITTING FROM BOTTOM, INBD LOWER HOLE IS CRACKED AT 5 O`CLOCK. HOLE WAS REPAIRED IAW SRM 53-41-12 PG 222 WITH FREEZE PLUG. THIS IS A CAT B REPAIR & REQUIRES SRI INSPECTION IAW SRM 53-41-12 TABLE 202 ON PAGE 203.

Part: SKIN — DEBONDED (RT ELEVATOR) · airframe 70,412 hrs · 26,285 cycles

RIGHT ELEVATOR UPPER SKIN HAS A DISBOND 23" FROM INBD, 25" FROM TE, 2" DIA. REMOVED UNBONDED AREA & APPLIED REPAIR IAW SRM 55-21-11 PARA 5E.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,412 hrs · 26,285 cycles

R2 DOOR SILL HAS CORROSION AT NUTPLATE AT FRAME 68. REPAIRED IAW SRM 53-41-14 FIGURE 201 SHEET 3 PRINCIPLE 4.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,412 hrs · 26,285 cycles

R2 DOOR SILL HAS CORROSION AT NUTPLATE AT FRAME 68. REPAIRED IAW SRM 53-41-14 FIGURE 201 SHEET 3 PRINCIPLE 4 ON HAECO NR 35080.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,237 hrs · 24,972 cycles

CORROSION FOUND ON SEAT TRACK AT Y 1292 AT FRAME 20 WAS OUT OF SRM LIMITS. SEAT TRACK REPLACED FROM FRAME 12 - FRAME 24 IAW SRM 51-44-11 & 51-42-11.

Part: FASTENER — MISSING (FUSELAGE) · airframe 67,032 hrs · 24,893 cycles

TWO FASTENERS MISSING ON PNL NEXT TO PNL 191KB. REPLACED TWO FASTENERS NEXT TO PNL 191KB.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 66,795 hrs · 24,805 cycles

LEVEL 1 CHRONIC LAVATORY SMOKE DETECTOR FAULT. REPEAT GRIPES FOR LAVATORY SMOKE DETECTOR FAULT ASSOCIATED WITH LAVATORY F 6WQ FAILURE MESSAGE. SMOKE DETECTOR IN LAVATORY F R & R DUE HISTORY.

Part: SDAC — FAULTY (COCKPIT) · airframe 66,787 hrs · 24,802 cycles

SDAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN, RESET NO HELP. SWAP SDAC 1 & 2, NOTE MRS IAW AMM 31-55-34-401, PCN 482-9503. UNABLE TO RESET SDAC 1, SWAPPED WITH SDAC 1 & APPLIED MEL IAW AMM 31-55-34-401. SDAC 2 IS NOW INOPERATIVE. SDAC 1 TESTED NORMAL. STICKER APPLIED NEXT TO LOWER ECAM. NR 2 SDAC IAW MM31-55-34-400 -001-A,31-50-00-710-001-A, IPC31-54-08-02A, MR31541-149 NR 1 POSITION & MR31541-103 NR 2 POSITION.

Part: UNKNOWN — MALFUNCTIONED (CARGO HEAT) · airframe 66,624 hrs · 24,739 cycles

CARGO HEAT ZONE CONT FAILS TO SEND SIGNAL TO HOT AIR VLV TO OPEN. NO HEAT TO PIT. DEACTIVATED TRIM AIR VLV IAW MEL, POST FLIGHT REPORT FAILURE MESSAGE NO AFT CHC DATA.

Part: SWITCH — MALFUNCTIONED (HYDRAULIC SYS) · airframe 66,604 hrs · 24,732 cycles

IAW SMC06 BLUE SYSTEM CHECK FAIL PER A-CHECK JOB CARD 4-2025 STEP 23D ITEM E4. CHECKED POWER TO SOL VLV GOOD ANOTHER VLV ON ORDER. VERIFIED SOL VLV BAD, PART COMING FROM DEN OSTF U2694. REPLACED HYD LEAK MAINTENANCE SWITCH IAW AWD29-19-01 PG 11, GND OPERATIONS CHECKED OKAY.

Part: SOLENOID VALVE — FAULTY (HYDRAULIC SYS) · airframe 66,604 hrs · 24,732 cycles

IAW A CHECK JOB CARD 4-2025. ITEM 23 RUDDER HYD ACT OPERATION CHECKED STEP E4. WHEN THE LEAK MEASURE B IS SELECTED THE B INDICATION ON ECAM STAYS GREEN & DOES NOT TURN AMBER. REPLACED SOLENOID VLV PCN 644-0070 IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 65,965 hrs · 24,489 cycles

SEAT ROW 21ABC OVERWING DOOR LOWER EMERGENCY EXIT LIGHT BROKEN. REPLACED OVERWING DOOR LOWER EMERGENCY LIGHT AT SEAT ROW 21 ABC IAW A319-A320 AMM, OPERATIONS CHECKED OKAY.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 65,965 hrs · 24,489 cycles

SEAT ROW 29ABC SEAT EMERGENCY EXIT LIGHT MOUNTED EMERGENCY LIGHT INOPERATIVE. TROUBLESHOOTING FOUND SEAT 29A UNDER SEAT PLASTIC CONNECTOR, BLACK WIRE WILL NOT LOCK IN PLACE IN PLASTIC EMERGENCY CONNECTOR.

Part: UNKNOWN — FAULTY (CABIN) · airframe 65,959 hrs · 24,485 cycles

CABIN EMERGENCY LIGHT CHECK FAILED IAW ITEM 3, 2SV C CK INT LOADS EMERGENCY L & EXT LOADS EMERGENCY L FAULT. TRIED NEW POWER SUPPLY & BATTERY, NO HELP. INSTALLED ORIGINAL, CLEANED EXTERNAL EMERGENCY LIGHTS & SOCKETS, THEY ILLUMINATE BUT TEST FAILS. SLIDE NEEDS TO BE TESTED LT SIDE IAW TSM 33-51-00. MT33-001

Part: FASTENER — MISSING (NR 2 PYLON) · airframe 65,902 hrs · 24,468 cycles

SCREW UP ON NR 2 PYLON MISSING ONE UNDER BELLY BY RED BEACON ON PANEL. REPLACED MISSING FASTENERS.

Part: ARMREST — LOOSE (CABIN) · airframe 65,898 hrs · 24,467 cycles

ARMREST CONSOLE LOOSE AT 7F. PERFORMED AN INTERIM REPAIR IAW ECRA 2000-01279. REPLACED NEW ARMREST END CAP.

Part: HANDSET — DAMAGED (CABIN) · airframe 65,816 hrs · 24,435 cycles

FORWARD PASSENGER ADDRESS HANDSET CABLE IS DAMAGED & HANDSET IS INOPERATIVE. REPLACED HANDSET.

Part: COWLING — CORRODED (NR 2 ENGINE) · corrosion level 2 · airframe 65,767 hrs · 24,416 cycles

FOUND SURFACE CORROSION ON NR 2 ENGINE INLET COWL LEADING EDGE. CLEANED LIGHT SURFACE CORROSION FROM INLET COWL LEADING EDGE.

Part: NOSE COWL — DAMAGED (NR 2 ENGINE) · airframe 65,767 hrs · 24,416 cycles

NR 2 ENGINE OUTBOARD SIDE OF NOSE COWL HAS GROUND DAMAGE APPROXIMATELY 3X3 INCHES. SAMC TEXT: REPLACED NOSE COWL PER MM (MR71212) REMOVED & REPLACED NR 2 ENGINE NOSE COWL PER AMM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,584 hrs · 24,348 cycles

RIGHT EMERGENCY EPSU BATTERY FAULT LIGHT. REPLACED EPSU BATTERY IAW AMM.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 65,514 hrs · 24,315 cycles

RIGHT FUEL TANK ACCESS PANELS 650BB & 650DB HAVE ELONGATED HOLES AT TANK LANDINGS. REPAIR ACCOMPLISHED IAW ECRA 5720-02433.

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 65,514 hrs · 24,315 cycles

LEFT WING FUEL TANK ACCESS PANEL 540PB HAS 3 ELONGATED HOLES IN THE MANHOLE SURROUND LANDING. LANDINGS REPAIRED.

Part: CONTROL UNIT — MALFUNCTIONED (MLG) · airframe 65,497 hrs · 24,308 cycles

LGCIU NR 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED LGCIU NR 2 IAW MM32-31-71.

Part: CONTROL UNIT — MALFUNCTIONED (MLG) · airframe 65,495 hrs · 24,307 cycles

CREW REPORTED LG CIU 1 FAULT. REPLACED NR 1 LGCIU REF AMM. ACCOMPLISHED TEST, OK AND NO FAULTS DISPLAYED.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,375 hrs · 24,265 cycles

ROW 34 EMERGENCY PATH LIGHT INOPERATIVE ON SIDE OF SEAT. REPLACED LIGHT WIRE HARNESS.

Part: DIAPHRAGM — LOW PRESSURE (L2 DOOR ASSIST) · airframe 65,236 hrs · 24,212 cycles

FOUND L2 DOOR EMERGENCY DOOR ASSIST BOTTLE PRESSURE LOW. REPLACED DIAPHRAGM IN PERCUSSION MECHANISM OF DOOR DAMPER AND EMERGENCY OPS CYLINDER OF L2 DOOR.

Part: PANEL — LOOSE (CABIN) · airframe 65,000 hrs · 24,118 cycles

OXY MASK COMPARTMENT DOWN AT 31B. NOT O2 PANEL DROP. FILLER PANEL LOOSE. SECURED PANEL.

Part: OXYGEN BOTTLE — LOW PRESSURE (CABIN) · airframe 64,547 hrs · 23,942 cycles

O2 BOTTLE LAST ROW RIGHT SIDE LOW. REPLACED O2 BOTTLE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 64,286 hrs · 23,841 cycles

IDG 1 OIL OVERHEAT DISPLAYED ON UPPER ECAM.

Part: SKIN — DENTED (RT WING) · airframe 64,039 hrs · 23,748 cycles

DENTED RIGHT WING LEADING EDGE RIGHT WING BETWEEN ENGINE AND WINGTIP. REPAIRED IAW SRM 57-40-00.

Part: CONTROL UNIT — MALFUNCTIONED (NLG STEERING) · airframe 63,735 hrs · 23,634 cycles

LOST NLG STEERING ON TURN ONTO RWY. CREW REPORTS LOSS OF STEERING AFTER CAPTAIN`S HANDWHEEL INPUT. PFR SHOWS BSCU CH 2 FAULT. RESET WITH "2ND" NWS SWITCH RESET. RESET BSCU CH2 FAULT PER TSM 24-00-00 AND ACCP'S MCDU TEST SYSTEM PASSED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,640 hrs · 23,598 cycles

FWD LT AND AFT LT EPSU BATTERIES FAIL EMERGENCY LIGHT CHECK. REPLACED BATTERIES IAW MM, EMERGENCY LIGHT TEST OK.

Part: BATTERY — FAILED (CABIN) · airframe 63,640 hrs · 23,598 cycles

FWD LT AND AFT LT EPSU BATTERIES FAIL EMERGENCY LIGHT CHECK. REPLACED BATTERIES IAW MM, EMERGENCY LIGHT TEST OK.

Part: STARTER — LOCKED (NR 2 ENGINE) · airframe 63,608 hrs · 23,585 cycles

RAMP REPORTS SPARKS FROM NR 2 ON STARTUP. FOUND STARTER LOCKED, REPLACE STARTER REF AMM.

Part: ENGINE — MAKING METAL (NR 1) · airframe 63,547 hrs · 23,565 cycles

NR 1 ENGINE GEARBOX RT SCAVENGE CHIP DETECTOR IS COVERED WITH EXCESSIVE METAL DEBRIS. FOUND WHILE ACCOMPLISHING EM3677: FILTER REPLACED AND ENGINE DOUBLE FLUSH. WITH PROBE REMOVED, CHIP DET HOUSING WILL NOT SEAL DUE SO MUCH METAL DEBRIS. REMOVED NR 1 ENGINE PER MT71-017. REPLACED NR 1 ENGINE.

Part: ALTERNATOR — FAULTY (NR 1) · airframe 63,513 hrs · 23,552 cycles

1 ENGINE FADEC ALTERNATOR, ENGINE 1 STALL, ENGINE 1 SENSOR FAULT, ENGINE 1 FAIL ECAM, REPLACE DEDICATED ALTERNATOR DRIVE PER MM. REPLACED DEDICATED ALTERNATOR ROTOR ASSEMBLY PER MM. LEAK CHECK GOOD WITH EDA DRIVE. ENGINES 1 AND 2 SERVICED TO FULL AFTER ENGINE POWER RUN. REPLENISHED ENGINE OIL. OK FOR SERVICE.

Part: WIRE HARNESS — FAULTY (NLG STEERING) · airframe 63,254 hrs · 23,445 cycles

NW STEER FAULT DISPLAYED ON UPPER ECAM SCREEN. INDICATED A DUAL FAILURE OF THE STEERING ELECTRO-HYDRAULIC MODULE (6GC). CFDS TEST FAILED THIS UNIT ON INITIAL EVALUATION. REPLACED NOSE WHEEL STEERING SERVO CONTROL. DURING MEGGER CHECK OF WIRES FROM NORMAL SERVO VALVE 15GG TO BSCU (10GG) BENCH PLUG, FOUND WIRE BETWEEN PIN F OF 15GG AND PIN 9A ON AB CONNECTOR OF BSCU FAILS MEG CHECK. IT SHOWS SHORT UNDER 500V TEST. DISCONNECTED CONNECTOR 4029VC AND ISOLATED THE PROBLEM TO LEFT GEAR HARNESS BETWEEN CONNECTOR 4029VC AND VALVE 15GG. STARTED TO REMOVED HARNESS. REPLACED HARNESS AND BITE CHECKS ON MC DUE LCGU 1 AND LGCU 2 AND BSCU ONE AND TWO BITE CHECKS OK.

Part: CLAMP — LOOSE (ANTI ICE DUCT) · airframe 61,436 hrs · 22,771 cycles

ANTI-ICE VALVE LEAKING HOT AIR ONTO NOSE COWL CAUSING DELAMINATION OF NOSE COWL. NR 1 ENGINE ANTI-ICE VALVE FOUND ONE CLAMP NOT SECURED. THIS CAUSED THE AFT BULKHEAD HEAT SHIELD TO COME APART BEHIND THE ANTI-ICE VALVE.

Part: BLOWOUT PANEL — DAMAGED (CARGO BAY) · airframe 61,333 hrs · 22,732 cycles

AFT CARGO CEILING BLOW OUT PANEL DAMAGED AT EDGES. BLOWOUT PANEL DAMAGED, NO REPAIR PERMITTED. NEEDS 110-4970 (RAPID FIX). REPLACED AFT PIT BLOW OUT PANEL PER MM.

Part: UNKNOWN — ODOR (CABIN) · airframe 60,482 hrs · 22,418 cycles

F/A REPORT AN ELECTRICAL ODOR WHEN PACKS ARE TURNED ON WITH APU PROVIDING AIR. RAN PACK 2 WITH AC DOOR CLOSE AND NO ODOR NOTICED.

Part: ATTACH FITTING — DEFECTIVE (CABIN) · airframe 60,430 hrs · 22,398 cycles

CREW REPORT: 31ABC WHOLE ROW OFF TRACKS. REPLACED THE AFT ATTACH FITTING SECURED SEAT.

Part: FITTING — MISSING (EVAC SLIDE) · airframe 60,326 hrs · 22,350 cycles

DOOR 1L, SLIDE COVER TO SLIDE-RAFT HAS BROKEN LOCK SECURING STRAP FROM BOTTOM SLIDE COVER TO SLIDE- RAFT. AFT SIDE OF SLIDE COVER. REPLACED MISSING CLIP AFT SLIDE STRAP AT DOOR 1L.

Part: SLIDE — UNWANTED DEPLOY (R2 DOOR) · airframe 59,994 hrs · 22,202 cycles

R2 DOOR SLIDE DEPLOYED. DEPLOYED SLIDE HAS BEEN REMOVED.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 59,809 hrs · 22,118 cycles

CAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. REPLACED O2 MASK ASSY.

Part: HYDRAULIC SYSTEM — LEAKING (BLUE SYSTEM) · airframe 59,467 hrs · 21,978 cycles

WHILE WORKING RAT OPERATIONAL CHECK, FOUND BLUE MANIFOLD SYSTEM LEAKING HYDRAULIC FLUID STEADY STREAM. RAT NEEDS TO BE STOWED AFTER BLUE HYD GROUND LEAKAGE-MEASUREMENT MANIFOLD REPLACEMENT.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 59,446 hrs · 21,968 cycles

RIGHT MAIN LANDING GEAR GREEN SYSTEM LEAKING. LINE PCN 110-1084 ETA 0740 CSC. REPLACED LOCK STAY HOSE. VERIFIED SAFETY WIRE INSTALLATION AND NO LEAKS AFTER PRESSURE CHECK.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 59,400 hrs · 21,952 cycles

DOOR 1L WILL NOT ARM. CLEANED DEBRIS FROM LOWER DOOR SILL ARMS AS REQUIRED.

Part: DRAIN LINE — OPEN (HYDRAULIC SYS) · airframe 59,200 hrs · 21,877 cycles

YELLOW HYD SYS ECAM, RTFL. FOUND YELLOW SYS HYD PRESS DRAIN OPEN AND PORTING AIR OVERBOARD, THIS WOULD GET YOU A LOW PRESS LT. RESERVICED YELLOW SYS AND OPS SYS. YELLOW SYS OPS NORMAL.

Part: IGNITER — FAULTY (APU) · airframe 59,161 hrs · 21,860 cycles

CREW REPORT: APU INOP. NO START 3 TIMES IN A ROW. CREW REPORT: APU INOP. NO START 3 TIMES IN A ROW SAMC TEXT: APU LAST LEG REPORT AND SHUT DOWN REPORTS SHOW IGN UNIT 8030KM AND FUEL CONTROL 8022KM, RESET L41 AND L42 NO HELP. LCL MAINT COMPLIED WITH MEL4910B, CB'S L41 AND L42 PULLED AND COLLARED USING DEFER STICKERS, OPB R ON NOTIFIED, WORK ACCOMPLISHED BY LCL MAINT. -INF- :NEXT MAINT STATION (DEN FL T.317-01JUL11) PLEASE REPLACE DEFER STICKERS WITH REGULAR CIRCUIT BREAKERS COLLARS AT L41 AND L42 ON 121VU PANEL. REPLACED BURNED IGNITERS AND IGNITER LEADS. STARTED APU OK.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 59,057 hrs · 21,822 cycles

EMERGENCY LIGHT TEST FAILED WITH MESSAGE. REPLACED OVERWING POWER SUPPLY AND BATTERY, NO HELP, NOW HAVE INTERNAL LOADS AND EXTERNAL LOADS FAULT, LIGHTS AT SEAT, ROWS 23, 29, 35,3 6, 37 DO NOT LIGHT UP. REPLACED LT POWER SUPPLY UNIT AND BATTERY. GOT "INT LIGHT FAULT". REPLACED LIGHT ASSY AT SEAT 29. SEAT 35, 36, 37 OP-CHECK SATISFACTORY. FOUND BROKEN WIRE AT SEAT 23. DEFERRED DUE TIME. ONLY SEAT 23 LIGHT IS INOPERATIVE, STOWED WIRES.

Part: SKIN — DENTED (NR 4 SLAT) · airframe 58,441 hrs · 21,584 cycles

ON WALK AROUND APPARENT DENT ON NR 4 SLAT RT SIDE. SLAT REPAIRED PER SRM 57-40-00. OKAY FOR SERVICE.

Part: PANEL — DAMAGED (NR 2 ENGINE) · airframe 58,005 hrs · 21,428 cycles

ACCOUSTICAL PANEL DAMAGE AT NR 2 ENG. REPLACED RT TRANSLATING COWL ON NR 2 ENGINE. OPS CHECKED REF MM. NO FAULTS NOTED.

Part: OXYGEN MASK — FAILED (COCKPIT) · airframe 56,831 hrs · 20,922 cycles

PILOT'S SIDE O2 MASKS NEED TO BE REINSTALLED. REPLACED MASK ON ACCOUNT IT WAS FAILING TEST.

Part: TRANSMITTER — LEAKING (O2 REGULATOR) · airframe 56,822 hrs · 20,918 cycles

CREW O2 STILL LEAKING. LOST 60PSI IN 50 MINUTES OF FLIGHT. REPLACED 02 PRESSURE REGULATOR TRANSMITTER, LEAK CKD, NO LEAKS FOUND.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 56,820 hrs · 20,917 cycles

OXYGEN PRESSURE STILL SLOWLY DECREASING. FOUND O2 MASK LEAKING AT QUICK DISCONNECT FITTING IN 1ST OBSERVER POSITION. REPLACED MASK OPS AND LEAK CHECKED GOOD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,150 hrs · 20,621 cycles

AFT PIT BILGE STR 41R IS CORRODED BETWEEN FRAMES 58 AND FRAME 59 BASE N-R D6219Y. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. DAMAGE FOUND OUT OF LIMITS. REMOVED DAMAGED SECTION OF STRINGER. ACP NDT OF CUT ENDS NO DEFECTS. FABRICATED & INSTALLED REPAIR STRINGER & 2 EA STRINGER SPLICES.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,150 hrs · 20,621 cycles

AFT PIT BILGE STR 43L AFT OF FRAME 56 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION, OUT OF LIMITS. FABRICATED FILLER AND INSTALLED.

Part: SKIN — DAMAGED (E&E BAY DOOR) · airframe 56,150 hrs · 20,621 cycles

FWD NOSE E & E COMPT DOOR SKIN DAMAGED. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW FWD E & E DOOR SKIN.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,150 hrs · 20,621 cycles

FWD PIT BILGE STRINGER CORRODED FROM FR 31 TO 33, STR 41L. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. INSTALLED REINFORCING ANGLE REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,150 hrs · 20,621 cycles

AFT PIT BILGE, STR 43L CORRODED BETWEEN FR 58 AND 60. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGED STR AT FWD COUPLING AND AT AFT END AT FACTORY SPLICE. INSTALLED NEW COUPLINGS FWD AND AFT ENDS.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 56,150 hrs · 20,621 cycles

INTERNAL FRAME 5 LT SIDE EXPERIENCED TOOLING DAMAGE DURING INSTALLATION OF PREVIOUS DOUBLER REPAIR ABOVE STATIC PORT. REMOVED & REPLACED FRAME NR 5 FROM BELOW CAPTAINS WINDOW TO JUST BELOW SKIN LAP.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 56,150 hrs · 20,621 cycles

INTERNAL FRAME 4 LT SIDE EXPERIENCED TOOLING DAMAGE DURING INSTALLATION OF PREVIOUS DOUBLER REPAIR ABOVE STATIC PORT. R & R FRAME NR4 FROM BELOW CAPTAIN'S WINDOW TO JUST BELOW SKIN LAP.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 56,150 hrs · 20,621 cycles

AFT PIT BILGE STR SPLICE ON STR 43L BETWEEN FR 56 AND 57 IS CORRODED. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW SPLICE.

Part: STRINGER — CORRODED (STR 41R) · airframe 56,150 hrs · 20,621 cycles

MAJOR REPAIR. FWD PIT BILGE STRINGER SPLICE ON STRINGER 41R BETWEEN FRAMES FR29 AND FRAME 30 IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION AND EVALUATED DAMAGE. FOUND CORROSION OUT OF LIMITS. FARBICATED & INSTALLED NEW STRINGER SPLICE.

Part: STRINGER — CORRODED (STR 43R) · airframe 56,150 hrs · 20,621 cycles

MAJOR REPAIR. FWD PIT BILGE STRINGER 43R IS CORRODED BETWEEN FRAMES FR30 AND FRAME 31. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION AND EVALUATED DAMAGE. FOUND CORROSION OUT OF LIMITS. FARBICATED & INSTALLED REPAIR ANGLE.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,150 hrs · 20,621 cycles

LT AFT FUSELAGE EXTERNAL SKIN DENTED BETWEEN FRAMES FR78 & FR80 AT STRINGER 25L. MAJOR REPAIR ACCOMPLISHED & EVALUATED DENT. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN SECTION BETWEEN STRINGERS 25L & 29L. OBTAINED NEW SKIN PANEL & INSTALLED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,150 hrs · 20,621 cycles

AFT PIT STR 31 R AFT OF FR 64 IS 6 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW STR 31R.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,150 hrs · 20,621 cycles

SEAT TRACK CORRODED AT MAIN DECK FLOOR, FR 38 TO FR 41, + Y292 LT, 2 LOCATIONS. INSTALLED NEW SEAT TRACK.

Part: STRINGER — CORRODED (STR 41R) · airframe 56,150 hrs · 20,621 cycles

MAJOR REPAIR. FWD PIT BILGE STRINGER 41R IS CORRODED BETWEEN FRAMES FR29 AND FRAME 31. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION AND EVALUATED DAMAGE. FOUND CORROSION OUT OF LIMITS. FARBICATED & INSTALLED REPAIR ANGLE.

Part: POSITION SENSOR — OUT OF RIG (LT WING TE FLAP) · airframe 55,635 hrs · 20,395 cycles

FOUND LT WING APPU FLAP POSITION PICK OFF UNIT ASYMMETRY OUT OF RIG. ZERO MARK TO DRIVE SHAFT MARK AT FLAPS FULL UP. DRIVING GEAR ZERO MARK DOES NOT LINE UP WITH FIXED POINTER BY ABOUT ONE DRIVE SHAFT SPLINE. REPLACED LT WING APPU. OPS TEST OF THE FLAP SYS. SFCC-1&2 PPU DATA DEG LT & RT APPU & FPPU SAME. CHECKED THAT ALL SYNCHRO ANGLES WITHIN LIMITS IAW MM AFTER LT APPU WAS REPLACED. NO FAULTS ON ECAM.

Part: PANEL — CRACKED (WING) · airframe 55,503 hrs · 20,333 cycles

FOUND CRACK IN L/E RT PANEL 621BB. REPLACED 621BB PANEL.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 53,671 hrs · 19,494 cycles

FUEL CALC ISSUES, FLT DIVERTED. CHECKED PFR'S NO MESSAGES. BITE TEST ON FAC. NO MESSAGES. RESET FUEL QTY LEVELS. DRIP STICK LEVELS MATCH. INITIALIZED MCDU TO LGA AND MATCHES ROUTE TO LGA. CONFIRMED WITH SAMC. AIRCRAFT FUEL SYSTEM, OPS NORMAL. NO PROBLEMS FOUND.

Part: ATTACH FITTING — CRACKED (EVAC SLIDE) · airframe 53,263 hrs · 19,315 cycles

DOOR 1L LWR FWD ATTACH FITTING IS CRACKED. REPLACED SLIDE.

Part: DOUBLER — OUT OF TOLERANCE (FUSELAGE) · airframe 53,263 hrs · 19,315 cycles

REPAIR DOUBLER BELOW NR 2 LT MED - FRAME 65 TO FRAME 66 STR 22LT TO 24 LT OUT OF TOLERANCE. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING DOUBLER AND INSTALLED NEW DOUBLER PICKING UP ONE ROW AFT OF SPLICE.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 53,263 hrs · 19,315 cycles

DENT WITHIN RVSM AREA AT FR4 & 5 LT SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: CABLE — OUT OF POSITION (EVAC SLIDE) · airframe 53,263 hrs · 19,315 cycles

DOOR 2R SLIDE PACK CAME UNDONE ON REMOVAL BECAUSE RELEASE CABLE WAS PINCHED BEHIND LINER. REPLACED SLIDE & INSPECTED.

Part: ATTACH FITTING — BROKEN (EVAC SLIDE) · airframe 53,263 hrs · 19,315 cycles

DOOR 1R SLIDE LWR FWD ATTACH FITTING BROKEN. REMOVED & REPLACED SLIDE RAFT.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,263 hrs · 19,315 cycles

FUSELAGE DENT APPROX 6 INCHES AFT OF FR 64 STR 23L. MAJOR REPAIR ACCOMPLISHED. EVALUATED DENT & FOUND OUT OF LIMITS. CUT OUT DAMAGE AND FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 52,547 hrs · 19,021 cycles

ENGINE HYDRAULIC PUMP FAILURE. RTFL. REPLACED NR 1 ENG HYD PUMP. ALSO REPLACED ENG PUMP CASE DRAIN FILTER AND HP FILTER. BOTH FILTERS CHECK NORMAL.

Part: HYDRAULIC LINE — LEAKING (GREEN SYSTEM) · airframe 52,089 hrs · 18,845 cycles

GREEN HYD LOSS. FLIGHT DIVERTED. CREW REPORTED, SHUT THE GREEN HYD SYSTEM OFF BEFORE COMPLETE LOSS OF HYD, STILL HAD 2.5 GALLONS IN RSVR. FOUND THE GREEN PRESSURE LINE LOCATED IN THE NR 1 ENG PYLON SWEDGE LEAKING. REPLACED LEAKING LINE. SERVICED GREEN SYSTEM TO FULL. LANDING GEAR RETURNED TO NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,037 hrs · 18,827 cycles

SEAT MOUNTED EVAC LIGHTS INOP AT SEAT 14 AND 23 ASSYS BROKEN. WILL NEED TWO. RELAMPED 23 AND REPLACED LIGHT ASSY AT 14. OPS CHECK OKAY.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 50,892 hrs · 18,392 cycles

SHEAR PLATE AFT OF DOOR 2R LOCATED BETWEEN FRAMES 68 AND 69 CRACKED. REPLACED TRAY.

Part: PLATE — CORRODED (FUSELAGE) · airframe 50,892 hrs · 18,392 cycles

SHEAR PLATE AFT OF DOOR 2R LOCATED BETWEEN FRAMES 69 AND 70 HEAVILY CORRODED. CONTINUED INSTALLATION OF SHEAR PLATE.

Part: PLATE — CORRODED (FUSELAGE) · airframe 50,892 hrs · 18,392 cycles

PLATE UNDER SHEAR PLATE LOCATED BETWEEN FRAME 69 AND 70 RIGHT SIDE OF AIRCRAFT CORRODED. REMOVED PLATE AND FWD ATTACH ANGLE.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 50,892 hrs · 18,392 cycles

LT DOOR SILL DOUBLER OUTBOARD HAS 2 CRACKS (MARKED). MAJOR REPAIR ACCOMPLISHED. REPLACED SILL SHAPE (DOUBLER), AT DOOR 2L.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,892 hrs · 18,392 cycles

FLOORBEAM 200 HAS TWO SMALL SPOTS OF CORROSION (MARKED). MAJOR REPAIR ACCOMPLISHED. STARTED REPLACING BEAM.

Part: SILL — CORRODED (FUSELAGE) · airframe 50,892 hrs · 18,392 cycles

LT DOOR SILL HAS SEVERAL AREAS OF CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED SILL SHAPE FROM SILL PLATE AT DOOR 2L. INSTALLED NEW SILL SHAPE ON SILL PLATE. NEEDS 2 FASTNERS DRILLED AND INSTALLED ON SHAPE. REPLACED 3 FASTENERS ON SILL SHAPE. REMOVED CORROSION ON SILL PLATE, PRIMED AND PAINTED.

Part: SILL — CORRODED (FUSELAGE) · airframe 50,892 hrs · 18,392 cycles

RT AFT DOOR SILL HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED 2R DOOR SILL. PICKING UP FASTENER HOLES, STARTED ASSY CLIPS AND PARTS. ASSEMBLED CLIPS AND CORNER CASTINGS, AND SERRATED PLATES TO SILL PAN. INSTALLED FASTENERS IN UPPER ROW OF SKIN, AND FWD FRAME. CONTINUED TO INSTALL FASTENERS LWR ROW OF SKIN AND COMMON TO (PARTIAL). INSTALLED REMAINING FASTENERS. NEED TO INSTALL FWD SPLICE ANGLES.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 50,226 hrs · 18,139 cycles

UPON ARRIVAL AT GATE NR 1 ENGINE WAS SMOKING HEAVILY.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 49,950 hrs · 18,037 cycles

LEFT UNIT DISPLAYED ON 3SV EMERGENCY LIGHT TEST. FOUND FAULTY BATTERY PACK. REPLACED EMERGENCY LIGHT BATTERY PACK & UNIT AT LT OVERWING. MESSAGE NO LONGER DISPLAYED. OK FOR SERVICE.

Part: OXYGEN SYSTEM — LEAKING (CREW) · airframe 49,925 hrs · 18,027 cycles

CREW O2 LEAKS 10 PSI EVERY 8 MINUTES.

Part: OXYGEN SYSTEM — LOW PRESSURE (CREW O2) · airframe 49,190 hrs · 17,773 cycles

CREW OXYGEN SYSTEM LOW. RECORD PRESS PRIOR TO SERVICING.

Part: UNKNOWN — VIBRATION (AIRFRAME) · airframe 48,548 hrs · 17,554 cycles

AFTER TAKEOFF, THE FLIGHT EXPERIENCED AIRFRAME VIBRATIONS UPON FLAP RETRACTION. STOPPED AFTER LEVEL OFF AND CONTINUED TO DESTINATION. PERFORMED SEVERAL FLAP TESTS, ACCOMPLISHED EFCS1 & EFCS2 ELEVATOR DAMPING AND AILERON DAMPING TEST -NO FAULTS NOTED OPERATIONAL CHECK OK. NO FAULTS NOTED AUTOLAND TEST ACCOMPLISHED SYS CHECKS OK.

Part: CONTROL UNIT — FAILED (COCKPIT) · airframe 48,483 hrs · 17,535 cycles

FLIGHT DIVERTED WITH AUTOPILOT PROBLEMS. POSSIBLE FMGC/FCU FAILURE. REPLACED FMGC/FCU COMBO. SYSTEM CHECKS NORMALLY, RESTORED TO CAT III STATUS.

Part: COVER — UNSECURE (R2 DOOR SLIDE) · airframe 48,459 hrs · 17,527 cycles

THE 2R SLIDE COVER FELL OFF AGAIN. PREVIOUS DAMAGE TO COVER. REPAIRED SLIDE COVER.

Part: INDICATION SYS — MALFUNCTIONED (FUEL QTY) · airframe 46,818 hrs · 16,950 cycles

FLIGHT DIVERTED DUE TO LOSS OF FUEL QUANTITY INDICATIONS FOR THE RIGHT WING. REPLACED CADENSCION.

Part: UNKNOWN — UNKNOWN (NR 2 ENGINE) · airframe 46,788 hrs · 16,937 cycles

PYLON ISSUES MANDATE NR 2 ENG REPLACEMENT.

Part: COMPUTER — FAULTED (NR 2 ELAC SYS) · airframe 46,700 hrs · 16,905 cycles

ELAC 2 FAULT DISPLAYED ON LOWER ECAM. 10-19-07 FOUND ELAC NR 2 FAULT. REPLACED AND RESET ELAC 2 AND ACP AFS TEST- NO REPEATS SINCE ORIGINAL.

Part: UNKNOWN — UNKNOWN (TE FLAPS) · airframe 46,398 hrs · 16,781 cycles

FLIGHT DIVERTED DUE TO FLAPS LOCKED MESSAGE DISPLAYED. PERFORMED WTB PROCEDURE PER TSM AND FLAPS RESET AND PERFORMED NORMALLY. NO REPEATS SINCE ORIGINAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,208 hrs · 16,711 cycles

FWD FACING AISLE, OVERHEAD-OVERWING EMERGENCY EXIT SIGN HAS SEVERAL BULBS INOP. RELAMPED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,208 hrs · 16,711 cycles

RED EMERGENCY PATH LIGHT AT SEAT 10C HAS ONE INOP LAMP. RELAMPED

Part: UNKNOWN — MALFUNCTIONED (TE FLAPS) · airframe 46,120 hrs · 16,676 cycles

FLAPS WOULD NOT GO TO FLAPS 2 WHEN SELECTED. RECEIVED A FLAPS LOCK MESSAGE. FLAPS WOULD NOT LEAVE FLAPS 1. TROUBLESHOOTING PER TSM REVEALED NO FAULTS. NO REPEATS.

Part: LIGHT — NO TEST (CABIN) · airframe 44,484 hrs · 16,079 cycles

EMERGENCY LIGHT TEST FAULTED LEFT UNIT. REPLACED EPSU. OPS CHECKS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,067 hrs · 15,927 cycles

DURING EMERGENCY LIGHT TEST FOUND MESSAGE UNIT EMER L. REPLACED BATTERY PACK AT DOOR 1L. OPS CHECKED GOOD.

Part: STARTER — FAILED (NR 1 ENGINE) · airframe 43,199 hrs · 15,627 cycles

FOUND START FAULT DISPLAYED ON UPPER ECAM SCREEN, NR 1 ENG. GROUND CREW CALLED. SPARKS AND GRINDING NOISE PRIOR TO 35PCT N1. SECOND ATTEMPT HAD NO ROTATE. INSPECT AREA SURROUNDING STARTER & START VALVE, REPLACE STARTER AND START VALVE. OPS CHECK GOOD.

Part: ENGINE — FLAMED OUT (NR 1) · airframe 42,408 hrs · 15,330 cycles

NR 1 ENGINE FLAMED OUT. CREW WAS ABLE TO RELIGHT AND TURNBACK. ENGINES RUNNING NORMAL.

Part: SLIDE — FAULTY (DOOR 2L) · airframe 41,499 hrs · 15,004 cycles

FOUND DOOR 2L ESCAPE SLIDE IS DEPLOYED BUT NOT INFLATED. THIS ESCAPE SLIDE SLIPPED OUT OF ITS POSITION BUT DID NOT DEPLOY. ON SITE INVESTIGATION REVEALED SAFETY PIN WAS IN PLACE, HOWEVER, SAFETY PIN FELL DOWN ON GRD AFTER HANGING FROM A/C FOR ABOUT 30 MINUTES. AFTER 30 MINUTES SLIDE SLOWLY DEPLOYED BEING IN THAT CONDITION. BOTTLE PRESSURE WAS ALSO FOUND BELOW GREEN BAND. REPLACED DIAPHRAM AND SERVICED BOTTLE . REMOVED AND REPLACED SLIDE.

Part: SKIN — DAMAGED (DOOR 1L) · airframe 39,465 hrs · 14,271 cycles

DOOR 1L HAS SKIN DAMAGE. MAJOR REPAIR OF DOOR SKIN PER SRM 52-10-00 FIGURE 203 WITH INCLUSION OF CORNER PRINCIPLE FROM FIGURE 205.

Part: TUBE — DAMAGED (ESCAPE SLIDE) · airframe 38,231 hrs · 13,868 cycles

3 IN LONG SLICE ON LOWER TUBE. SLICE OR LACERATION ON THE INFLATABLE TUBE COULD BE DUE TO MISHANDLING DURING UNIT TRANSPORTATION. THE DAMAGE WAS REPAIRED AND RETESTED OK.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,642 hrs · 12,016 cycles

LEFT FUSE SKIN IS CREASED & DENTED AT STA 359 (FR 23), STR 22L. MAJOR REPAIR ACCOMPLISHED. REPAIR ACCOMPLISHED PER MAE EA 47-5381-13-A1053 & UAL EVA IMC 30150.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,624 hrs · 12,008 cycles

FUSELAGE SKIN DENTED FROM FRAME 23 TO FRAME 24 BETWEEN STRINGERS 21L & 23L. DIMENSIONS ARE LENGTH 24.8 INCHES BY 10 INCHES HEIGHT WITH 5 SMALLER SHARP EDGES. MAJOR REPAIR ACCOMPLISHED. REPLACED STR 22L & FABRICATED EXTERNAL DOUBLER REPAIR UTILIZING SHIMS & FILLERS.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 32,624 hrs · 12,008 cycles

AFT PIT STRINGER 43 LT CORRODED BETWEEN FRAMES 56 & 57. MAJOR REPAIR ACCOMPLISHED. EXTRUDED STRINGER REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 32,624 hrs · 12,008 cycles

AFT CARGO COMPARTMENT STRINGER 42 LEFT CORRODED BETWEENN FRAMES 59 & 60. MAJOR REPAIR ACCOMPLISHED. EXTRUDED STRINGER SPLICE REPAIR.

Part: STRUCTURE — CONTAMINATED (LT ELEVATOR) · airframe 32,624 hrs · 12,008 cycles

LOWER PANEL OF LT ELEVATOR FOUND WITH WATER INGRESSION IN AREA APROX 1.5 BY 1.4 INCHES LOCATED APPROXIMATELY 2 IN FROM I/B EDGE AND 33 INCHES FROM TRAILING EDGE. MAJOR REPAIR ACCOMPLISHED. A REINFORCING REPAIR WAS ACCOMPLISHED PER SRM 55-21-11. REPAIR NR 5D ON PG 219 USING FIG 204 SHEET NR 2.

Part: SWITCH — FAULTY (HYDRAULIC SYS) · airframe 27,311 hrs · 9,936 cycles

DIVERTED TO MIA DUE TO HYDRAULIC QUANTITY LOSS INDICATION. CONFIRMED GREEN SYSTEM HYDRAULIC QUANTITY RESERVOIR FULL, NO EXTERNAL LEAKS NOTED. REPLACED LOW LEVEL SENSOR.

Part: LIGHT — INOPERATIVE (ROW 20) · airframe 22,774 hrs · 8,329 cycles

SEAT EMERGENCY ESCAPE PATH LIGHT INOPERABLE ROW 20. REPLACED SEAT LIGHT ASSY.

Part: LIGHT — FAILED TEST (CABIN)

AFT CABIN EMERGENCY LIGHTS FAIL TEST. MESSAGE IS INTERNAL LOADS EMER LT. TEST OF AFT CABIN EMERGENCY LIGHTS FAILED BUT TEST PASTED AT THE NEXT STATION.

Part: STARTER — SMOKED (NR 1 ENGINE)

NR 1 ENG STARTER BLEW SPARKS AND SMOKE DURING START AT PUSHBACK.

Part: SEAT — CRACKED (CABIN)

THIS IS THE FIRST HEAVY MAINTENANCE VISIT FOR THIS AIRCRAFT (HMV-1). VIRTUALLY 100 PERCENT OF THE SEAT PANS ON THE RECARO MODEL 3410, 720 SERIES PASSENGER SEATS WERE FOUND CRACKED.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHT TEST FAILED. MESSAGE LEFT COM, EXTERNAL FAULT CODE ON EPSU.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHT TEST GAVE A FAILED INDICATION DURING TESTING. *S/D* REPLACED FORWARD EMERGENCY BATTERY PACK AT FORWARD OVERHEAD DOOR 1 LEFT.

Part: DOOR SENSOR — MALFUNCTIONED (LANDING GEAR)

CREW REPORTED, AT THE OUTER MARKER THE GEAR WAS SELECTED DOWN AND THE INDICATIONS REMAINED RED. THE GEAR WAS RECYCLED AND OPERATED NORMALLY. *S/D* ACCOMPLISHED CHECK OF DOOR SENSORS AND WIRING. SWUNG GEAR SEVERAL TIMES AND COULD NOT DUPLICATE PROBLEM. SYSTEM OPERATIONALLY CHECKED GOOD WITH NO FURTHER PROBLEMS.

Part: PROXIMITY SENSOR — OUT OF ADJUST (RT MLG DOOR)

DURING GEAR EXTENSION ON ARRIVAL AT SFO, LANDING GEAR UNLOCK LIGHTS ILLUMINATED WITH NO GREEN DOWN AND LOCKED INDICATION. RECYCLED GEAR HANDLE AND GEAR EXTENDED NORMALLY. SUPPLEMENTAL DATA: UPDATE FOUND RIGHT HAND LANDING GEAR DOOR PROXIMITY SENSOR OUT OF ADJUSTMENT. ADJUSTED SENSOR, SWUNG GEAR AND OPERATED NORMALLY.

Part: DOWNLOCK IND — MALFUNCTIONED (LANDING GEAR)

ON SHORT FINAL, GEAR SELECTED DOWN, DID NOT RECEIVE GEAR LOCKED INDICATION LIGHT. RECYCLED GEAR LEVER AND GEAR LOCKED. HEARD GURGLING SOUND FROM CENTER CONSOLE. FIRST OFFICER'S PFD AND ND WENT BLANK AND THEN CAME BACK UP WITH NO PILOT ACTION. *S/D* COULD NOT DUPLICATE PROBLEM ON GROUND. REPLACED GEAR DOOR SENSOR 38GA AND LANDING GEAR SELECTOR VALVE PRECAUTIONARY, SYSTEM CHECKED NORMAL.

Part: ELEVATORS — OUT OF TOL (LT/RT)

CREW REPORTS HIGH SPEED BUFFET, WHEN SPEED IS BETWEEN 305 AND 320 KNOTS AT FLIGHT LEVEL 28.0, APPEARS TO GO AWAY WHEN SPEED DROPS BELOW 300 KNOTS. REPLACED BOTH ELEVATORS AND THS ACTUATOR.

Part: EEL — INOPERATIVE (CABIN)

INTERIOR EMERGENCY EXIT LIGHTS OUT AT DOOR 1 LEFT AND 1 RIGHT.